Avia 305 Study guides, Class notes & Summaries

LU AVIA 305 Quiz 4 • Question 1 In Subsonic flight the air is considered to be • Question 2 2.5 out of 2.5 points A Normal shock wave will have what effect on velocity and Mach number? • 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 • Question 4 2.5 out of 2.5 points A "stable" aircraft wing design is one where the

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...

New AVIA 305 QUIZ Aircraft Performance • Question 1 The power-required curves for an increase in altitude show that the • Question 2 The equation Ta=Q(V2-V1) shows that

An airplane is towing a glider to altitude. The tow rope is 20° below the horizontal and has a tension force of 300 lb exerted on it by the airplane. Find the horizontal drag of the glider and the amount of lift that the rope is providing to the glider. Sin 20° = 0.342; cos 20 °= 0.940.Drag: Cos 20° = D/T (Rearrange) D = Cos 20° X Tension D = 0.940 X 300lbs D = 282lbs Lift: Sin 20° = L/T (Rearrange) Lift = Sin 20° X Tension Lift = 0.342 X 300 lbs

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 difference between the CL curves for straight-wing aircraft is that a) the swept wing aircraft has a lower value of CL (max) b) the straight wing aircraft does not fly at as high an AOA for CL (max) c) the swept wing aircraft does not have an abrupt loss of lift at CL (max) d) all of the above d) all of the above Low speed stall will start at the wing's trailing edge a) where C1/C2 is a minimum b) where C1/C2 is a maximum c) at the root for a swept wing d) at the wingtip for a st...

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...