At116 - Study guides, Class notes & Summaries

AT116 Exam 2 2022 Study Guide with Complete Solutions Why would we want anhedral on a wing? - Answer-The a/c has a very heavy and low center of gravity Which of the following is NOT one of the ways an airplane gains stability around vertical axis? - Answer-Move CG behind center of lift How do we create yaw stability on an a/c? - Answer-Only a & b are correct Put a vertical stabilizer on tail of a/c Sweep wings back What produces pitch stability on a standard a/c? - Answer-Both b & c are...

AT116 TEST 1 STUDY GUIDE WITH COMPLETE SOLUTIONS what are standard conditions - Answer-59 degrees Sea level Zero humidity 41 degrees N Lat. •By 18,000 feet____ of all the air on the planet is below you. By 34,000 feet _____ of all the air is below you. - Answer-•By 18,000 feet 50 of all the air on the planet is below you. By 34,000 feet 75 of all the air is below you. air temp falls at a constant rate until ___________ - Answer-36,000 ft what happens to static pressure as he aera o...

AT116 Exam 2 Study Guide with Complete Solutions Load Factor - Answer-ratio of the total load supported by the wing compared to the weight of the aircraft. Also commonly known as "G force". Load Factor Equation - Answer-load supported by wing/total weight of aircraft Positive Static Stability - Answer-initial tendency to return to the position from which it was displaced Neutral Static Stability - Answer-The initial tendency of the aircraft to remain in a new condition after its equili...

AT 116 EXAM 2 QUESTIONS WITH 100% VERIFIED ANSWERS...

AT 116 FINAL COMPLETE EXAM WITH QUESTIONS AND VERIFIED ANSWERS...

AT 116 Exam 2 Questions and Answers |100% Pass 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...

AT 116 TEST 2 QUESTIONS WITH ANSWERS ...

AT 116 Test 2 Questions and Answers |100% Pass 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...

AT 116 Exam Study Questions and Answers |100% Pass Which is true with respect to the density of the air? a. Air is less dense when there is high humidity b. Air is more dense when there is high humidity c. Density stays the same - Answer-a. Which is true with respect to the density of the air? a. The air density (air pressure) at 18,000 feet is about 1/2 of the density at sea level b. The air density (air pressure) at 34,000 feet is about 1/2 of the density at sea level c. The air densi...