Anhedral angle - Study guides, Class notes & Summaries
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ASTB-E Exam Prep 2023 with 100% correct answers
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Airfoil - correct answer A wing or helicopter blade that generates more lift than drag as air flows over its upper and lower surfaces. They are carefully designed and can be made of non-metallic materials such as composites. 
 
Angle of attack - correct answer The angle between the chord line of an airfoil and its direction of motion relative to the air (i.e., the relative wind). It is an aerodynamic angle. 
 
Angle of incidence - correct answer In the context of fixed-wing airplanes, the angle ...
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ASTB-E exam 2023 with 100% correct answers
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Pressure Altimeter - correct answer in the cockpit is automatically calibrated for 29.92 inches of mercury. 
Pilot resets the pressure altitude indicator after departing an airfield to ensure correct pressure altitude 
 
Fuselage - correct answer main section that holds the crew, passengers, and cargo 
 
Monocoque Structure - correct answer a thin sheet-aluminum alloy curved to fit the shell of the fuselage. It is designed to withstand the stress of loads and minimize the total weight ...
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AFOQT Aviation| 208 Questions with 100% correct answers.
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what is an airfoil 
anything designed to produce lift when it moved through the air 
 
 
 
Cantilever wing 
sufficient internal support structures to keep it steady in its location 
 
 
 
Two designations of wings 
Cantilever or semi-cantilever 
 
 
 
Semi-Cantilever wings 
requires additional external support structures 
 
 
 
Flaps 
run from the fuselage to the middle of the wing 
 
 
 
Ailerons 
Run from the middle of the wing to the tip. responsible for the roll, or movement around the longi...
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AFOQT (Pilot) Q&A VEIFIED 100%
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AFOQT (Pilot) Q&A VEIFIED 100% 
Distance from one wingtip to another wingtip - ANSWER wingspan 
What is an airfoil - ANSWER anything designed to produce lift when it 
moved through the air 
Cantilever wing - ANSWER sufficient internal support structures to keep it 
steady in its location 
Two designations of wings - ANSWER Cantilever or semi-cantilever 
Cantilever wings - ANSWER sufficient internal support structures to keep 
it steady in its location 
Semi-Cantilever wings - ANSWER requires ...
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AFOQT Pilot EXAM PRETEST QUESTIONS ANSWERED CORRECTLY
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AFOQT Pilot EXAM PRETEST QUESTIONS 
ANSWERED CORRECTLY 
2 Types of Aviation - ANSWER Civilian & Military 
Fixed Wing Examples - ANSWER Fighter jets, bombers, civilian jets and 
corporate airliners 
Rotary-Wing Examples - ANSWER Helicopters, gyro-copters, and tilt-rotor 
flying machines 
Aircraft - ANSWER Machine supported aloft by lift created by air flowing 
across airfoil, wings, propeller, rotor blades or buoyancy 
Civilian Aircraft categorized as - ANSWER normal, utility, acrobatic, 
co...
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Aero 321 Final Exam 45 Questions with Verified Answers,100% CORRECT
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Aero 321 Final Exam 45 Questions with Verified Answers 
 
Equation of motion assumptions ( &when bad) - CORRECT ANSWER All internal forces are in equilibrium 
Constant gravity (bad for orbit) 
Flat earth (bad for long flights) 
Constant mass(bad for rockets) 
Rigid body( bad for supersonic cruisers) 
 
Inertial Coupling - CORRECT ANSWER -Results from imbalances in inertia 
-Start with pitching equation, rearrange for pitch acceleration 
 
Gyroscopic Coupling - CORRECT ANSWER Spinning rotors, red...
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AT 116 Exam 2 Questions and Answers |100% Pass
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AT 116 Exam 2 Questions and Answers 
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T/F Wing dihedral is one of the ways that we achieve stability around the longitudinal axis - Answer- 
True 
E: Roll stability on a low wing aircraft is corrected using a dihedral wing angle. In normal flight the 
Bernoulli effect (lift) does not pull straight up, it pulls up and in-board. 
If the aircraft rolls, one wing is directly opposing weight, while the other is slanted. This allows the wing 
to roll back into level flight. 
T/F Wing dihedr...
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AT 116 Test 2 Questions and Answers |100% Pass
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AT 116 Test 2 Questions and Answers 
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If an aircraft has positive STATIC stability, which is true of the aircraft? 
a - The aircraft attempts to return to straight and level but constantly over shoots and continues to 
oscillate at a constant rate 
b - The aircraft does not display any tendency to return to straight and level but stays at whatever 
attitude it is 
placed. 
c - Displays a tendency to want to return to straight and level. 
d - The aircraft does not remain at straight an...
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ASTB-E Exam Prep Already Graded To Pass!!
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ASTB-E Exam Prep Already Graded To Pass!!
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AFOQT Study Guide (Aviation Information) Questions and Answers 2023
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AFOQT Study Guide (Aviation Information) Questions and Answers 2023 
Flaps 
Location: Aft/ Trailing Edge 
Purposes: (1) Increase lift by deflecting airflow downward (2) When extended, increases surface area (3) Decreases velocity required for takeoff and landing 
 
 
 
Slats 
Location: Leading Edge 
Purposes: Maintain lift at low speeds when extended 
 
 
 
Spoilers 
Location: On the wings of many turbine-powered aircraft 
Purpose: Destroy the residual lift after landing, putting the planes enti...
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