From 9d577bcc3774a70d7dfb53cb9ba68a995dfb208b Mon Sep 17 00:00:00 2001 From: Matthias Nott <mnott@mnsoft.org> Date: Sun, 12 Apr 2026 21:04:23 +0200 Subject: [PATCH] Update references. --- SPL Exam Questions EN/80 - Principles of Flight.md | 264 ++++++++++++++++++++++++++-------------------------- 1 files changed, 132 insertions(+), 132 deletions(-) diff --git a/SPL Exam Questions EN/80 - Principles of Flight.md b/SPL Exam Questions EN/80 - Principles of Flight.md index 19dc73a..226dc43 100644 --- a/SPL Exam Questions EN/80 - Principles of Flight.md +++ b/SPL Exam Questions EN/80 - Principles of Flight.md @@ -51,7 +51,7 @@ #### Source -- Examen Blanc: [VV Q30 p.217](Questionnaire%20toutes%20branches%20VV.pdf#page=217) (score: 0.24) +- [VV Q30 p.217](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=217) (score: 0.24) - PDF Answer: D ### Q3: After one wing stalls and the nose drops, what is the correct technique to prevent a spin? ^t80q3 @@ -151,7 +151,7 @@ #### Source -- Examen Blanc: [VV Q52 p.64](Questionnaire%20toutes%20branches%20VV.pdf#page=64) (score: 0.23) +- [VV Q52 p.64](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=64) (score: 0.23) - PDF Answer: D ### Q7: What purpose does the vertical tail fin (rudder assembly) serve? ^t80q7 @@ -176,7 +176,7 @@ #### Source -- Examen Blanc: [VV Q52 p.222](Questionnaire%20toutes%20branches%20VV.pdf#page=222) (score: 0.25) +- [VV Q52 p.222](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=222) (score: 0.25) - PDF Answer: D ### Q8: In a coordinated level turn at 60 degrees of bank, the load factor is approximately ^t80q8 @@ -274,7 +274,7 @@ #### Source -- Examen Blanc: [S1S Q16 p.42](Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.27) +- [S1S Q16 p.42](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.27) - PDF Answer: C ### Q12: In straight and level flight, what happens to the required angle of attack as speed increases? ^t80q12 @@ -304,7 +304,7 @@ #### Source -- Examen Blanc: [VV Q21 p.184](Questionnaire%20toutes%20branches%20VV.pdf#page=184) (score: 0.23) +- [VV Q21 p.184](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=184) (score: 0.23) - PDF Answer: B ### Q13: What is the function of wing fences or boundary layer fences? ^t80q13 @@ -397,7 +397,7 @@ #### Source -- Examen Blanc: [VV Q36 p.187](Questionnaire%20toutes%20branches%20VV.pdf#page=187) (score: 0.29) +- [VV Q36 p.187](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=187) (score: 0.29) - PDF Answer: D ### Q17: What does the term "load factor" describe? ^t80q17 @@ -426,7 +426,7 @@ #### Source -- Examen Blanc: [VV Q13 p.77](Questionnaire%20toutes%20branches%20VV.pdf#page=77) (score: 0.24) +- [VV Q13 p.77](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=77) (score: 0.24) - PDF Answer: A ### Q18: How does increasing aircraft weight affect the best glide ratio? ^t80q18 @@ -470,7 +470,7 @@ #### Source -- Examen Blanc: [VV Q20 p.78](Questionnaire%20toutes%20branches%20VV.pdf#page=78) (score: 0.21) +- [VV Q20 p.78](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=78) (score: 0.21) - PDF Answer: C ### Q20: What is the effect of extending airbrakes (spoilers) on a glider? ^t80q20 @@ -495,7 +495,7 @@ #### Source -- Examen Blanc: [S2 Q18 p.27](Exa%20Blanc%20Série_2.pdf#page=27) (score: 0.25) +- [S2 Q18 p.27](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=27) (score: 0.25) ### Q21: In which flight condition is induced drag greatest? ^t80q21 @@ -520,7 +520,7 @@ #### Source -- Examen Blanc: [S1S Q13 p.41](Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.22) +- [S1S Q13 p.41](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.22) - PDF Answer: A ### Q22: What is the primary function of an elevator trim tab? ^t80q22 @@ -568,7 +568,7 @@ #### Source -- Examen Blanc: [S1S Q18 p.42](Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.31) +- [S1S Q18 p.42](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.31) - PDF Answer: C ### Q24: What is the centre of pressure of an aerofoil? ^t80q24 @@ -595,7 +595,7 @@ #### Source -- Examen Blanc: [VV Q15 p.214](Questionnaire%20toutes%20branches%20VV.pdf#page=214) (score: 0.24) +- [VV Q15 p.214](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=214) (score: 0.24) - PDF Answer: D ### Q25: At what point during flight is parasite drag greatest? ^t80q25 @@ -621,7 +621,7 @@ #### Source -- Examen Blanc: [VV Q50 p.64](Questionnaire%20toutes%20branches%20VV.pdf#page=64) (score: 0.21) +- [VV Q50 p.64](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=64) (score: 0.21) - PDF Answer: B ### Q26: What is the Bernoulli principle as applied to an aerofoil? ^t80q26 @@ -773,7 +773,7 @@ #### Source -- Examen Blanc: [VV Q19 p.183](Questionnaire%20toutes%20branches%20VV.pdf#page=183) (score: 0.25) +- [VV Q19 p.183](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=183) (score: 0.25) - PDF Answer: D ### Q32: What is the purpose of a laminar-flow aerofoil? ^t80q32 @@ -821,7 +821,7 @@ #### Source -- Examen Blanc: [VV Q30 p.113](Questionnaire%20toutes%20branches%20VV.pdf#page=113) (score: 0.28) +- [VV Q30 p.113](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=113) (score: 0.28) - PDF Answer: D ### Q34: What is the difference between static stability and dynamic stability? ^t80q34 @@ -889,7 +889,7 @@ #### Source -- Examen Blanc: [VV Q95 p.231](Questionnaire%20toutes%20branches%20VV.pdf#page=231) (score: 0.22) +- [VV Q95 p.231](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=231) (score: 0.22) - PDF Answer: B ### Q37: In which direction does the centre of pressure move as the angle of attack increases (pre-stall)? ^t80q37 @@ -915,7 +915,7 @@ #### Source -- Examen Blanc: [VV Q16 p.214](Questionnaire%20toutes%20branches%20VV.pdf#page=214) (score: 0.40) +- [VV Q16 p.214](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=214) (score: 0.40) - PDF Answer: C ### Q38: What determines the critical angle of attack at which a wing stalls? ^t80q38 @@ -968,7 +968,7 @@ #### Source -- Examen Blanc: [VV Q171 p.143](Questionnaire%20toutes%20branches%20VV.pdf#page=143) (score: 0.22) +- [VV Q171 p.143](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=143) (score: 0.22) - PDF Answer: C ### Q40: Which types of drag make up total drag? ^t80q40 @@ -1020,8 +1020,8 @@ #### Source -- Examen Blanc: [S2 Q18 p.27](Exa%20Blanc%20Série_2.pdf#page=27) (score: 0.24) -- [QuizVDS Q41](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q41): Answer A +- [S2 Q18 p.27](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=27) (score: 0.24) +- [QuizVDS Q41](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q41): Answer A ### Q42: To recover from a stall, it is essential to ^t80q42 @@ -1081,8 +1081,8 @@ #### Source -- Examen Blanc: [VV Q19 p.183](Questionnaire%20toutes%20branches%20VV.pdf#page=183) (score: 0.20) -- [QuizVDS Q41](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q41): Answer A +- [VV Q19 p.183](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=183) (score: 0.20) +- [QuizVDS Q41](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q41): Answer A - PDF Answer: D ### Q44: The critical angle of attack ^t80q44 @@ -1114,8 +1114,8 @@ #### Source -- Examen Blanc: [VV Q48 p.221](Questionnaire%20toutes%20branches%20VV.pdf#page=221) (score: 0.26) -- [QuizVDS Q44](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q44): Answer C +- [VV Q48 p.221](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=221) (score: 0.26) +- [QuizVDS Q44](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q44): Answer C - PDF Answer: D ### Q45: What leads to a lower stall speed Vs (IAS)? ^t80q45 @@ -1150,8 +1150,8 @@ #### Source -- Examen Blanc: [VV Q19 p.183](Questionnaire%20toutes%20branches%20VV.pdf#page=183) (score: 0.21) -- [QuizVDS Q45](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q45): Answer B +- [VV Q19 p.183](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=183) (score: 0.21) +- [QuizVDS Q45](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q45): Answer B - PDF Answer: D ### Q46: Which statement about a spin is correct? ^t80q46 @@ -1200,8 +1200,8 @@ #### Source -- Examen Blanc: [S1S Q17 p.42](Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.25) -- [QuizVDS Q47](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q47): Answer B +- [S1S Q17 p.42](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.25) +- [QuizVDS Q47](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q47): Answer B - PDF Answer: C ### Q48: What types of boundary layers are found on an aerofoil? ^t80q48 @@ -1295,7 +1295,7 @@ #### Source -- Examen Blanc: [S1S Q2 p.40](Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.82) +- [S1S Q2 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.82) - PDF Answer: D ### Q52: During a sideslip, the permitted flap position is ^t80q52 @@ -1318,7 +1318,7 @@ #### Source -- Examen Blanc: [S1S Q15 p.42](Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.65) +- [S1S Q15 p.42](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.65) - PDF Answer: A ### Q53: An aircraft is said to have dynamic stability when ^t80q53 @@ -1341,7 +1341,7 @@ #### Source -- Examen Blanc: [S1S Q19 p.43](Exa%20Blanc%20Série_1_Specifiques.pdf#page=43) (score: 0.88) +- [S1S Q19 p.43](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=43) (score: 0.88) - PDF Answer: A ### Q54: In severe turbulence, airspeed must be reduced ^t80q54 @@ -1364,7 +1364,7 @@ #### Source -- Examen Blanc: [VV Q19 p.78](Questionnaire%20toutes%20branches%20VV.pdf#page=78) (score: 0.22) +- [VV Q19 p.78](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=78) (score: 0.22) - PDF Answer: D ### Q55: In the ICAO standard atmosphere, the temperature lapse rate in the troposphere is ^t80q55 @@ -1391,7 +1391,7 @@ #### Source -- Examen Blanc: [S1S Q1 p.40](Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.70) +- [S1S Q1 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.70) - PDF Answer: D ### Q56: At approximately what altitude does atmospheric pressure fall to half its sea-level value? ^t80q56 @@ -1417,7 +1417,7 @@ #### Source -- Examen Blanc: [S1S Q3 p.40](Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.54) +- [S1S Q3 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.54) - PDF Answer: C ### Q57: Density altitude always corresponds to ^t80q57 @@ -1444,7 +1444,7 @@ #### Source -- Examen Blanc: [S1S Q4 p.40](Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.66) +- [S1S Q4 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.66) - PDF Answer: C ### Q58: The simplified continuity law applied to an airflow states: *In a given period of time, a flowing air mass is conserved regardless of the cross-section it passes through.* This means that ^t80q58 @@ -1472,7 +1472,7 @@ #### Source -- Examen Blanc: [S1S Q5 p.40](Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.70) +- [S1S Q5 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.70) - PDF Answer: A ### Q59: The aerodynamic resultant (drag and lift) depends on air density. When air density decreases ^t80q59 @@ -1500,7 +1500,7 @@ #### Source -- Examen Blanc: [S1S Q6 p.40](Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.52) +- [S1S Q6 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.52) - PDF Answer: A ### Q60: What is the name of the point about which, when the angle of attack changes, the pitching moment around the lateral axis does not vary? ^t80q60 @@ -1526,7 +1526,7 @@ #### Source -- Examen Blanc: [S1S Q11 p.41](Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.65) +- [S1S Q11 p.41](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.65) - PDF Answer: D ### Q61: The angle between the aerofoil chord line and the aircraft's longitudinal axis is called ^t80q61 @@ -1553,7 +1553,7 @@ #### Source -- Examen Blanc: [S1S Q9 p.41](Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.56) +- [S1S Q9 p.41](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.56) - PDF Answer: D ### Q62: What does the transition point correspond to? ^t80q62 @@ -1576,7 +1576,7 @@ #### Source -- Examen Blanc: [S1S Q17 p.42](Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.65) +- [S1S Q17 p.42](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.65) - PDF Answer: C ### Q63: Geometric or aerodynamic wing twist results in ^t80q63 @@ -1599,7 +1599,7 @@ #### Source -- Examen Blanc: [S1S Q10 p.41](Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.61) +- [S1S Q10 p.41](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.61) - PDF Answer: B ### Q64: The profile drag (form drag) of a body is primarily influenced by ^t80q64 @@ -1622,7 +1622,7 @@ #### Source -- Examen Blanc: [S1S Q14 p.42](Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.71) +- [S1S Q14 p.42](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.71) - PDF Answer: C ### Q65: The aerodynamic drag of a flat disc in an airflow depends notably on ^t80q65 @@ -1652,7 +1652,7 @@ #### Source -- Examen Blanc: [S1S Q12 p.41](Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.68) +- [S1S Q12 p.41](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.68) - PDF Answer: B ### Q66: On the speed polar, which tangent touches the curve at the point of minimum sink rate? ^t80q66 @@ -1686,7 +1686,7 @@ #### Source -- Examen Blanc: [S1S Q16 p.42](Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.55) +- [S1S Q16 p.42](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.55) - PDF Answer: C ### Q67: Induced drag increases ^t80q67 @@ -1719,7 +1719,7 @@ #### Source -- Examen Blanc: [S1S Q13 p.41](Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.33) +- [S1S Q13 p.41](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.33) - PDF Answer: A ### Q68: How does the minimum speed of an aircraft in a level turn at 45-degree bank compare to straight-and-level flight? ^t80q68 @@ -1746,7 +1746,7 @@ #### Source -- Examen Blanc: [S1S Q18 p.42](Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.33) +- [S1S Q18 p.42](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=42) (score: 0.33) - PDF Answer: C ### Q69: Adverse yaw is caused by ^t80q69 @@ -1769,7 +1769,7 @@ #### Source -- Examen Blanc: [S1S Q8 p.41](Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.59) +- [S1S Q8 p.41](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.59) - PDF Answer: D ### Q70: True Airspeed (TAS) is the speed shown by the ASI ^t80q70 @@ -1797,7 +1797,7 @@ #### Source -- Examen Blanc: [S1S Q7 p.41](Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.65) +- [S1S Q7 p.41](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.65) - PDF Answer: D ### Q71: The speed range authorised for the use of slotted flaps is: ^t80q71 @@ -1823,7 +1823,7 @@ #### Source -- Examen Blanc: [S2 Q1 p.37](Exa%20Blanc%20Série_2.pdf#page=37) (score: 0.43) +- [S2 Q1 p.37](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=37) (score: 0.43) ### Q72: Wing tip vortices are caused by pressure equalisation from: ^t80q72 @@ -1845,7 +1845,7 @@ #### Source -- Examen Blanc: [S2 Q2 p.37](Exa%20Blanc%20Série_2.pdf#page=37) (score: 0.33) +- [S2 Q2 p.37](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=37) (score: 0.33) ### Q73: The angle of attack of an aerofoil is always the angle between: ^t80q73 @@ -1871,8 +1871,8 @@ #### Source -- Examen Blanc: [S2 Q3 p.37](Exa%20Blanc%20Série_2.pdf#page=37) (score: 0.65) -- [QuizVDS Q14](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q14): Answer B +- [S2 Q3 p.37](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=37) (score: 0.65) +- [QuizVDS Q14](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q14): Answer B ### Q74: In the standard atmosphere, the values of temperature and atmospheric pressure at sea level are: ^t80q74 @@ -1907,7 +1907,7 @@ #### Source -- Examen Blanc: [S2 Q4 p.37](Exa%20Blanc%20Série_2.pdf#page=37) (score: 0.91) +- [S2 Q4 p.37](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=37) (score: 0.91) ### Q75: Regarding airflow, the simplified continuity equation states: At the same moment, the same mass of air passes through different cross-sections. Therefore: ^t80q75 @@ -1931,7 +1931,7 @@ #### Source -- Examen Blanc: [S3 Q20 p.41](Exa%20Blanc%20Série_3.pdf#page=41) (score: 0.42) +- [S3 Q20 p.41](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=41) (score: 0.42) ### Q76: In a correctly executed turn without altitude loss, why is slight back-pressure on the elevator necessary? ^t80q76 @@ -1953,7 +1953,7 @@ #### Source -- Examen Blanc: [S3 Q6 p.38](Exa%20Blanc%20Série_3.pdf#page=38) (score: 0.53) +- [S3 Q6 p.38](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=38) (score: 0.53) ### Q77: When the frontal area of a disc in an airflow is tripled, drag increases by: ^t80q77 @@ -1990,7 +1990,7 @@ #### Source -- Examen Blanc: [S2 Q7 p.38](Exa%20Blanc%20Série_2.pdf#page=38) (score: 0.64) +- [S2 Q7 p.38](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=38) (score: 0.64) ### Q78: Aerodynamic wing twist (washout) is a modification of: ^t80q78 @@ -2031,7 +2031,7 @@ #### Source -- Examen Blanc: [S2 Q8 p.38](Exa%20Blanc%20Série_2.pdf#page=38) (score: 0.75) +- [S2 Q8 p.38](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=38) (score: 0.75) ### Q79: What is the average value of gravitational acceleration at the Earth's surface? ^t80q79 @@ -2056,7 +2056,7 @@ #### Source -- Examen Blanc: [S1S Q2 p.40](Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.82) +- [S1S Q2 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.82) - PDF Answer: D ### Q80: The speed displayed on the airspeed indicator (ASI) is a measurement of: ^t80q80 @@ -2079,7 +2079,7 @@ #### Source -- Examen Blanc: [S2 Q10 p.38](Exa%20Blanc%20Série_2.pdf#page=38) (score: 0.72) +- [S2 Q10 p.38](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=38) (score: 0.72) ### Q81: The horizontal and vertical stabilisers serve in particular to: ^t80q81 @@ -2103,7 +2103,7 @@ #### Source -- Examen Blanc: [S2 Q11 p.38](Exa%20Blanc%20Série_2.pdf#page=38) (score: 0.36) +- [S2 Q11 p.38](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=38) (score: 0.36) ### Q82: When slotted flaps are extended, airflow separation: ^t80q82 @@ -2153,7 +2153,7 @@ #### Source -- Examen Blanc: [S2 Q13 p.39](Exa%20Blanc%20Série_2.pdf#page=39) (score: 0.89) +- [S2 Q13 p.39](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=39) (score: 0.89) ### Q84: Pressures are expressed in: ^t80q84 @@ -2175,7 +2175,7 @@ #### Source -- Examen Blanc: [S2 Q14 p.39](Exa%20Blanc%20Série_2.pdf#page=39) (score: 0.71) +- [S2 Q14 p.39](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=39) (score: 0.71) ### Q85: TAS (True Air Speed) is the speed of: ^t80q85 @@ -2200,7 +2200,7 @@ #### Source -- Examen Blanc: [S2 Q15 p.39](Exa%20Blanc%20Série_2.pdf#page=39) (score: 0.48) +- [S2 Q15 p.39](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=39) (score: 0.48) ### Q86: Yaw stability of an aircraft is provided by: ^t80q86 @@ -2222,7 +2222,7 @@ #### Source -- Examen Blanc: [S2 Q16 p.39](Exa%20Blanc%20Série_2.pdf#page=39) (score: 0.30) +- [S2 Q16 p.39](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=39) (score: 0.30) ### Q87: The trailing edge flap shown below is a: ^t80q87 @@ -2246,7 +2246,7 @@ #### Source -- Examen Blanc: [S2 Q16 p.39](Exa%20Blanc%20Série_2.pdf#page=39) (score: 0.39) +- [S2 Q16 p.39](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=39) (score: 0.39) ### Q88: The risk of airflow separation on the wing occurs mainly: ^t80q88 @@ -2268,7 +2268,7 @@ #### Source -- Examen Blanc: [S2 Q18 p.40](Exa%20Blanc%20Série_2.pdf#page=40) (score: 0.53) +- [S2 Q18 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=40) (score: 0.53) ### Q89: The drag of a body in an airflow depends notably on: ^t80q89 @@ -2295,7 +2295,7 @@ #### Source -- Examen Blanc: [VV Q5 p.212](Questionnaire%20toutes%20branches%20VV.pdf#page=212) (score: 0.40) +- [VV Q5 p.212](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=212) (score: 0.40) - PDF Answer: D ### Q90: In the drawing below, the aerofoil chord is represented by: ^t80q90 @@ -2337,7 +2337,7 @@ #### Source -- Examen Blanc: [S2 Q12 p.26](Exa%20Blanc%20Série_2.pdf#page=26) (score: 0.20) +- [S2 Q12 p.26](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=26) (score: 0.20) ### Q91: The angle of attack of an aerofoil is always measured between: ^t80q91 @@ -2370,8 +2370,8 @@ #### Source -- Examen Blanc: [S3 Q1 p.37](Exa%20Blanc%20Série_3.pdf#page=37) (score: 0.71) -- [QuizVDS Q14](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q14): Answer B +- [S3 Q1 p.37](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=37) (score: 0.71) +- [QuizVDS Q14](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q14): Answer B ### Q92: Given equal frontal area and equal airflow speed, what determines the drag of a body? ^t80q92 @@ -2402,7 +2402,7 @@ #### Source -- Examen Blanc: [S3 Q2 p.37](Exa%20Blanc%20Série_3.pdf#page=37) (score: 0.50) +- [S3 Q2 p.37](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=37) (score: 0.50) ### Q93: What is the origin of induced drag on a wing? ^t80q93 @@ -2428,7 +2428,7 @@ #### Source -- Examen Blanc: [S3 Q3 p.37](Exa%20Blanc%20Série_3.pdf#page=37) (score: 0.45) +- [S3 Q3 p.37](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=37) (score: 0.45) ### Q94: What is the sea-level pressure in the ICAO standard atmosphere? ^t80q94 @@ -2458,7 +2458,7 @@ #### Source -- Examen Blanc: [S3 Q4 p.37](Exa%20Blanc%20Série_3.pdf#page=37) (score: 0.58) +- [S3 Q4 p.37](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=37) (score: 0.58) ### Q95: In the aerofoil diagram below, which line represents the mean camber line? ^t80q95 @@ -2509,7 +2509,7 @@ #### Source -- Examen Blanc: [S3 Q6 p.38](Exa%20Blanc%20Série_3.pdf#page=38) (score: 0.45) +- [S3 Q6 p.38](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=38) (score: 0.45) ### Q97: A wing stall occurs: ^t80q97 @@ -2539,7 +2539,7 @@ #### Source -- Examen Blanc: [S3 Q7 p.38](Exa%20Blanc%20Série_3.pdf#page=38) (score: 0.43) +- [S3 Q7 p.38](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=38) (score: 0.43) ### Q98: At what condition does airflow separation from an aerofoil occur? ^t80q98 @@ -2568,7 +2568,7 @@ #### Source -- Examen Blanc: [S3 Q8 p.38](Exa%20Blanc%20Série_3.pdf#page=38) (score: 0.30) +- [S3 Q8 p.38](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=38) (score: 0.30) ### Q99: What is the mean gravitational acceleration at the surface of the Earth? ^t80q99 @@ -2597,7 +2597,7 @@ #### Source -- Examen Blanc: [S1S Q2 p.40](Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.73) +- [S1S Q2 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.73) - PDF Answer: D ### Q100: True Airspeed (TAS) is obtained from the airspeed indicator (ASI) reading by: ^t80q100 @@ -2630,7 +2630,7 @@ #### Source -- Examen Blanc: [S3 Q10 p.39](Exa%20Blanc%20Série_3.pdf#page=39) (score: 0.39) +- [S3 Q10 p.39](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=39) (score: 0.39) ### Q101: A shift of the centre of gravity is caused by: ^t80q101 @@ -2659,7 +2659,7 @@ #### Source -- Examen Blanc: [VV Q16 p.77](Questionnaire%20toutes%20branches%20VV.pdf#page=77) (score: 0.50) +- [VV Q16 p.77](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=77) (score: 0.50) - PDF Answer: C ### Q102: The high-lift device shown in the diagram is a: ^t80q102 @@ -2687,7 +2687,7 @@ #### Source -- Examen Blanc: [S3 Q12 p.39](Exa%20Blanc%20Série_3.pdf#page=39) (score: 0.30) +- [S3 Q12 p.39](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=39) (score: 0.30) ### Q103: The resultant of all aerodynamic forces on a wing profile acts through the: ^t80q103 @@ -2713,7 +2713,7 @@ #### Source -- Examen Blanc: [VV Q15 p.214](Questionnaire%20toutes%20branches%20VV.pdf#page=214) (score: 0.37) +- [VV Q15 p.214](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=214) (score: 0.37) - PDF Answer: D ### Q104: At approximately what altitude is the air density half of its sea-level value? ^t80q104 @@ -2743,7 +2743,7 @@ #### Source -- Examen Blanc: [S3 Q14 p.40](Exa%20Blanc%20Série_3.pdf#page=40) (score: 0.75) +- [S3 Q14 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=40) (score: 0.75) ### Q105: The airspeed indicator (ASI) reading is based on a measurement of: ^t80q105 @@ -2774,7 +2774,7 @@ #### Source -- Examen Blanc: [S2 Q10 p.38](Exa%20Blanc%20Série_2.pdf#page=38) (score: 0.63) +- [S2 Q10 p.38](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=38) (score: 0.63) ### Q106: Roll stability is influenced by: ^t80q106 @@ -2800,7 +2800,7 @@ #### Source -- Examen Blanc: [S3 Q16 p.40](Exa%20Blanc%20Série_3.pdf#page=40) (score: 0.64) +- [S3 Q16 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=40) (score: 0.64) ### Q107: The speed range for operating slotted flaps: ^t80q107 @@ -2830,7 +2830,7 @@ #### Source -- Examen Blanc: [S3 Q17 p.40](Exa%20Blanc%20Série_3.pdf#page=40) (score: 0.62) +- [S3 Q17 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=40) (score: 0.62) ### Q108: When the wing's angle of incidence is larger at the root than at the tip, this is called: ^t80q108 @@ -2859,7 +2859,7 @@ #### Source -- Examen Blanc: [S3 Q18 p.40](Exa%20Blanc%20Série_3.pdf#page=40) (score: 0.29) +- [S3 Q18 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=40) (score: 0.29) ### Q109: Barometric pressure in the Earth's atmosphere has the characteristic of: ^t80q109 @@ -2885,7 +2885,7 @@ #### Source -- Examen Blanc: [S3 Q18 p.40](Exa%20Blanc%20Série_3.pdf#page=40) (score: 0.31) +- [S3 Q18 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=40) (score: 0.31) ### Q110: The simplified continuity equation says the same mass of air passes through different cross-sections at the same instant. Therefore: ^t80q110 @@ -2911,7 +2911,7 @@ #### Source -- Examen Blanc: [S3 Q20 p.41](Exa%20Blanc%20Série_3.pdf#page=41) (score: 0.39) +- [S3 Q20 p.41](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=41) (score: 0.39) ### Q111: On the aerofoil diagram, what does point number 4 represent? ^t80q111 @@ -3017,8 +3017,8 @@ #### Source -- Examen Blanc: [S1S Q5 p.4](Exa%20Blanc%20Série_1_Specifiques.pdf#page=4) (score: 0.25) -- [QuizVDS Q53](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q53): Answer A +- [S1S Q5 p.4](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=4) (score: 0.25) +- [QuizVDS Q53](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q53): Answer A - PDF Answer: A ### Q115: Rotation about the vertical axis is termed ^t80q115 @@ -3045,8 +3045,8 @@ #### Source -- Examen Blanc: [S1S Q5 p.4](Exa%20Blanc%20Série_1_Specifiques.pdf#page=4) (score: 0.27) -- [QuizVDS Q56](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q56): Answer C +- [S1S Q5 p.4](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=4) (score: 0.27) +- [QuizVDS Q56](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q56): Answer C - PDF Answer: A ### Q116: Rotation about the lateral axis is termed ^t80q116 @@ -3073,8 +3073,8 @@ #### Source -- Examen Blanc: [VV Q75 p.69](Questionnaire%20toutes%20branches%20VV.pdf#page=69) (score: 0.27) -- [QuizVDS Q57](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q57): Answer B +- [VV Q75 p.69](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=69) (score: 0.27) +- [QuizVDS Q57](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q57): Answer B - PDF Answer: B ### Q117: The elevator causes the aircraft to rotate around the ^t80q117 @@ -3103,7 +3103,7 @@ #### Source -- Examen Blanc: [VV Q40 p.219](Questionnaire%20toutes%20branches%20VV.pdf#page=219) (score: 0.28) +- [VV Q40 p.219](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=219) (score: 0.28) - PDF Answer: C ### Q118: What must be considered regarding the centre of gravity position? ^t80q118 @@ -3293,8 +3293,8 @@ #### Source -- Examen Blanc: [VV Q26 p.185](Questionnaire%20toutes%20branches%20VV.pdf#page=185) (score: 0.20) -- [QuizVDS Q77](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q77): Answer C +- [VV Q26 p.185](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=185) (score: 0.20) +- [QuizVDS Q77](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q77): Answer C - PDF Answer: B ### Q125: The pressure equalisation between the upper and lower wing surfaces results in ^t80q125 @@ -3399,8 +3399,8 @@ #### Source -- Examen Blanc: [S2 Q7 p.38](Exa%20Blanc%20Série_2.pdf#page=38) (score: 0.23) -- [QuizVDS Q9](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q9): Answer B +- [S2 Q7 p.38](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=38) (score: 0.23) +- [QuizVDS Q9](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q9): Answer B ### Q129: In the diagram, what does number 3 represent? ^t80q129 @@ -3536,7 +3536,7 @@ #### Source -- Examen Blanc: [S1S Q6 p.40](Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.29) +- [S1S Q6 p.40](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=40) (score: 0.29) - PDF Answer: A ### Q134: Which combination of measures can improve the glide ratio of a sailplane? ^t80q134 @@ -3618,8 +3618,8 @@ #### Source -- Examen Blanc: [S1S Q5 p.4](Exa%20Blanc%20Série_1_Specifiques.pdf#page=4) (score: 0.22) -- [QuizVDS Q54](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q54): Answer B +- [S1S Q5 p.4](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=4) (score: 0.22) +- [QuizVDS Q54](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q54): Answer B - PDF Answer: A ### Q137: Which structural element provides directional stability? ^t80q137 @@ -3700,8 +3700,8 @@ #### Source -- Examen Blanc: [S1S Q5 p.4](Exa%20Blanc%20Série_1_Specifiques.pdf#page=4) (score: 0.22) -- [QuizVDS Q60](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q60): Answer B +- [S1S Q5 p.4](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=4) (score: 0.22) +- [QuizVDS Q60](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q60): Answer B - PDF Answer: A ### Q140: What happens when the rudder is deflected to the left? ^t80q140 @@ -3891,7 +3891,7 @@ #### Source -- Examen Blanc: [VV Q40 p.219](Questionnaire%20toutes%20branches%20VV.pdf#page=219) (score: 0.26) +- [VV Q40 p.219](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=219) (score: 0.26) - PDF Answer: C ### Q147: Which of the following factors causes the load factor to increase during cruise flight? ^t80q147 @@ -3921,8 +3921,8 @@ #### Source -- Examen Blanc: [VV Q66 p.225](Questionnaire%20toutes%20branches%20VV.pdf#page=225) (score: 0.21) -- [QuizVDS Q74](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q74): Answer D +- [VV Q66 p.225](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=225) (score: 0.21) +- [QuizVDS Q74](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q74): Answer D - PDF Answer: A ### Q148: While approaching the next updraft, the variometer shows 3 m/s descent. You expect a mean climb rate of 2 m/s in the thermal. How should you set the McCready ring? ^t80q148 @@ -4030,7 +4030,7 @@ #### Source -- Examen Blanc: [S1S Q9 p.41](Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.21) +- [S1S Q9 p.41](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=41) (score: 0.21) - PDF Answer: D ### Q152: In the figure, the angle (alpha) is referred to as ^t80q152 @@ -4085,8 +4085,8 @@ #### Source -- Examen Blanc: [VV Q41 p.219](Questionnaire%20toutes%20branches%20VV.pdf#page=219) (score: 0.29) -- [QuizVDS Q68](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q68): Answer B +- [VV Q41 p.219](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=219) (score: 0.29) +- [QuizVDS Q68](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q68): Answer B - PDF Answer: A ### Q154: What must be taken into account when flying a sailplane with water ballast? ^t80q154 @@ -4219,8 +4219,8 @@ #### Source -- Examen Blanc: [S3 Q2 p.37](Exa%20Blanc%20Série_3.pdf#page=37) (score: 0.23) -- [QuizVDS Q9](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q9): Answer B +- [S3 Q2 p.37](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_3.pdf#page=37) (score: 0.23) +- [QuizVDS Q9](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q9): Answer B ### Q159: "Longitudinal stability" refers to stability around which axis? ^t80q159 @@ -4246,8 +4246,8 @@ #### Source -- Examen Blanc: [S1S Q5 p.4](Exa%20Blanc%20Série_1_Specifiques.pdf#page=4) (score: 0.25) -- [QuizVDS Q53](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q53): Answer A +- [S1S Q5 p.4](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_1_Specifiques.pdf#page=4) (score: 0.25) +- [QuizVDS Q53](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q53): Answer A - PDF Answer: A ### Q160: What does "wing loading" mean? ^t80q160 @@ -4325,8 +4325,8 @@ #### Source -- Examen Blanc: [S2 Q18 p.27](Exa%20Blanc%20Série_2.pdf#page=27) (score: 0.26) -- [QuizVDS Q90](../../Examen%20Blanc/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q90): Answer B +- [S2 Q18 p.27](../SOURCES/Examen%20Blanc/Exa%20Blanc%20Série_2.pdf#page=27) (score: 0.26) +- [QuizVDS Q90](../SOURCES/QuizVDS/80%20-%20Principles%20of%20Flight.md#^q90): Answer B ### Q163: Does air density affect the minimum speed (IAS) of a glider? ^t80q163 @@ -4354,7 +4354,7 @@ #### Source -- Examen Blanc: [VV Q57 p.223](Questionnaire%20toutes%20branches%20VV.pdf#page=223) (score: 0.92) +- [VV Q57 p.223](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=223) (score: 0.92) - PDF Answer: C ### Q164: In which speed range can vibrations and flutter occur? ^t80q164 @@ -4383,7 +4383,7 @@ #### Source -- Examen Blanc: [VV Q27 p.185](Questionnaire%20toutes%20branches%20VV.pdf#page=185) (score: 0.33) +- [VV Q27 p.185](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=185) (score: 0.33) - PDF Answer: C ### Q165: Vibrations can occur when ^t80q165 @@ -4406,7 +4406,7 @@ #### Source -- Examen Blanc: [VV Q79 p.227](Questionnaire%20toutes%20branches%20VV.pdf#page=227) (score: 0.58) +- [VV Q79 p.227](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=227) (score: 0.58) - PDF Answer: A ### Q166: Vibrations can also occur under which conditions? ^t80q166 @@ -4429,7 +4429,7 @@ #### Source -- Examen Blanc: [VV Q80 p.228](Questionnaire%20toutes%20branches%20VV.pdf#page=228) (score: 0.56) +- [VV Q80 p.228](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=228) (score: 0.56) - PDF Answer: C ### Q167: In which speed range can the maximum load factor be exceeded, leading to structural overload? ^t80q167 @@ -4457,7 +4457,7 @@ #### Source -- Examen Blanc: [VV Q81 p.228](Questionnaire%20toutes%20branches%20VV.pdf#page=228) (score: 0.59) +- [VV Q81 p.228](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=228) (score: 0.59) - PDF Answer: B ### Q168: Above which speed can abrupt or full control deflections damage the glider's structure? ^t80q168 @@ -4480,7 +4480,7 @@ #### Source -- Examen Blanc: [VV Q83 p.228](Questionnaire%20toutes%20branches%20VV.pdf#page=228) (score: 0.93) +- [VV Q83 p.228](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=228) (score: 0.93) - PDF Answer: A ### Q169: When the maximum load factor is exceeded, what is the primary risk? ^t80q169 @@ -4503,7 +4503,7 @@ #### Source -- Examen Blanc: [VV Q31 p.186](Questionnaire%20toutes%20branches%20VV.pdf#page=186) (score: 0.53) +- [VV Q31 p.186](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=186) (score: 0.53) - PDF Answer: C ### Q170: The mass balance (mass balancing) of an aileron has lost lead weights. What can be the consequence? ^t80q170 @@ -4526,7 +4526,7 @@ #### Source -- Examen Blanc: [VV Q85 p.229](Questionnaire%20toutes%20branches%20VV.pdf#page=229) (score: 0.48) +- [VV Q85 p.229](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=229) (score: 0.48) - PDF Answer: B ### Q171: What is the danger of flying at minimum speed in turbulent air? ^t80q171 @@ -4549,7 +4549,7 @@ #### Source -- Examen Blanc: [VV Q92 p.230](Questionnaire%20toutes%20branches%20VV.pdf#page=230) (score: 0.79) +- [VV Q92 p.230](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=230) (score: 0.79) - PDF Answer: C ### Q172: How does air density change when temperature increases? ^t80q172 @@ -4578,7 +4578,7 @@ #### Source -- Examen Blanc: [VV Q94 p.231](Questionnaire%20toutes%20branches%20VV.pdf#page=231) (score: 0.55) +- [VV Q94 p.231](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=231) (score: 0.55) - PDF Answer: A ### Q173: In what proportion does drag change with airspeed? ^t80q173 @@ -4606,7 +4606,7 @@ #### Source -- Examen Blanc: [VV Q96 p.231](Questionnaire%20toutes%20branches%20VV.pdf#page=231) (score: 0.33) +- [VV Q96 p.231](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=231) (score: 0.33) - PDF Answer: D ### Q174: What is understood by static pressure? ^t80q174 @@ -4629,7 +4629,7 @@ #### Source -- Examen Blanc: [VV Q97 p.231](Questionnaire%20toutes%20branches%20VV.pdf#page=231) (score: 0.64) +- [VV Q97 p.231](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=231) (score: 0.64) - PDF Answer: C ### Q175: How does the maximum permissible speed Vne of a glider in IAS behave as altitude increases? ^t80q175 @@ -4659,7 +4659,7 @@ #### Source -- Examen Blanc: [VV Q20 p.78](Questionnaire%20toutes%20branches%20VV.pdf#page=78) (score: 0.67) +- [VV Q20 p.78](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=78) (score: 0.67) - PDF Answer: C ### Q176: In what proportion does lift change when airspeed increases? ^t80q176 @@ -4682,7 +4682,7 @@ #### Source -- Examen Blanc: [VV Q104 p.233](Questionnaire%20toutes%20branches%20VV.pdf#page=233) (score: 0.23) +- [VV Q104 p.233](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=233) (score: 0.23) - PDF Answer: B ### Q177: Which statement is FALSE regarding the relationship between lift/drag and airspeed? ^t80q177 @@ -4705,7 +4705,7 @@ #### Source -- Examen Blanc: [VV Q105 p.233](Questionnaire%20toutes%20branches%20VV.pdf#page=233) (score: 0.63) +- [VV Q105 p.233](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=233) (score: 0.63) - PDF Answer: C ### Q178: What is understood by total pressure? ^t80q178 @@ -4734,5 +4734,5 @@ #### Source -- Examen Blanc: [VV Q106 p.233](Questionnaire%20toutes%20branches%20VV.pdf#page=233) (score: 0.83) +- [VV Q106 p.233](../SOURCES/VV/Questionnaire%20toutes%20branches%20VV.pdf#page=233) (score: 0.83) - PDF Answer: C -- Gitblit v1.3.1