Avia 305 test 1 Study guides, Class notes & Summaries

AVIA 305 TEST 1 2021/2022 Correct answers are hidden. Score for this quiz: 65 out of 75 Submitted Jan 21 at 7:33pm This attempt took 53 minutes. IncorrectQuestion 1 0 / 2.5 pts A slotted flap is an example of a(n) (Ref Figure 1) Camber changer Energy adder Area changer A & B Question 2 2.5 / 2.5 pts

LU AVIA 305 Test 3 • 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. For a safe takeoff, the Critical Field Length must be no greater than the runway available An increase in density altitude has what effect on takeoff performance

AVIA 305 Test 3 • Question 1 Which statement is true with respect to Lift Coefficient (CL) and the Effect of Sweepback on Coefficient of Lift - Angle of Attack (AOA) curves. • Question 2 For a safe takeoff, the Critical Field Length must be no greater than the runway available • Question 3 An...

AVIA 305 Review Test Submission: Test 1 Attempt Score 57.5 out of 75 points • • Question 1 An airplane is operating from an airfield that has a barometric pressure of 28.86 in. Hg and a runway temperature of 20C. Calculate (or find in Table 2.1) the Temperature Ratio: • Question 2 The corrections that must be made to indicated airspeed (IAS) to obtain calibrated airspeed (CAS) are: • Question 3 A large Reynolds number (greater than 10 million) indicates • Question 4 An airplane is oper...

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

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

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...