Avia 305 Study guides, Class notes & Summaries

AVIA 305 Quiz: Maneuvering Performance Score for this quiz: 72.5 out of 75 Fall 2023 Score for this quiz: 72.5 out of 75 During a right crosswind landing in a tricycle gear airplane, a coordinated touchdown on the wheel first will mitigate side loading and prevent ground looping the aircraft. right left nosewheel tailwheel During a setup to a power-on stall in a single-engine propeller airplane, as IAS decreases additional input will be required to maintain coordinated flight. ri...

The equation Ta = Q (V2 - V1) shows thatyou can get more thrust from a jet engine by using water injection. you can get more thrust from a jet engine by decreasing the exhaust pipe area. Q in Ta = Q (V2 - V1) is the mass flow (slugs/sec). The mass flow depends onthe cross‐ sectional area of the turbojet engine inlet. the engine inlet velocity. the density of the air at the same point.

AVIA305 Aircraft Performance QUIZ (Questions and Answers)

AVIA 305 TEST 2 2021/2022 AVIA 305 Test 2 User Course LUO Test Test 2 Status Completed Attempt Score 67.5 out of 75 points • Question 1 2.5 out of 2.5 points The thrust available from a jet engine at 35,000 ft altitude compared to that at sea level is Selected Answer: Less • Question 2 If the weight of a jet airplane is increased then 2.5 out of 2.5 points Selected Answer: Induced drag increases more than parasite drag • Question 3 An example of a power-producing airc...

AVIA 305 TEST 3 2021/2022 • Question 1 2.5 out of 2.5 points Which statement is true with respect to Lift Coefficient (CL) and the Effect of Sweepback on Coefficient of Lift - Angle of Attack (AOA) curves. Selected Answer: • Question 2 All of the above 2.5 out of 2.5 points For a safe takeoff, the Critical Field Length must be no greater than the runway available Selected Answer: • Question 3 True 0 out of 2.5 points An increase in density altitude has what effect on takeo...

AVIA 305 TEST 4 2021/2022 Cours e LUO Test Test 4 Starte d ● ● Question 1 2.5 out of 2.5 points In Subsonic flight the air is considered to be Selected Answer: Incompressibl e ● Question 2 2.5 out of 2.5 points A Normal shock wave will have what effect on velocity and Mach number? Selected Answer: Decrease to subsonic ● Question 3 2.5 out of 2.5 points Aircraft speeds where the airflow around the aircraft ranges between Mach 0.7 and Mach 1.3 is Selected Answer:...

AVIA 305 Airplane Aerodynamics Test 1-Score for this quiz: 65 out of 75 (Liberty University)

AVIA 305/ AVIA305 Test 2; Attempt Score 67.5 out of 75 points..Complete solution 2020/2021

Liberty University Online Academy > AVIA 305/ AVIA305 Test 2; Attempt Score 67.5 out of 75 points