Avia 305 test - Study guides, Class notes & Summaries

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/ 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

AVIA 305 Test 3 (solved) fall 2021 (1).pdf

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

User Course Fall 2020 AVIA 305-D01 LUO Test Test 2 Status Completed Attempt Score 67.5 out of 75 points

AVIA 305 Test 3 (solved) fall 2021.

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