Climbing Flight

Question 1

During climb, pitch angle is the sum of __ angle and angle of attack

Answer 1

climb, attack

Question 2

Climbing at constant pitch and max climb thrust without a supercharger, gamma ___, AoA ___, IAS ___

Answer 2

decreases, increases, decreases

Question 3

For shallow flight path angles in straight and steady flight, the following formula can be used ___

Answer 3

Sin( gamma ) = ( T / W ) - ( Cd / Cl )

Question 4

Vx and Vy with take off flap will be ___ than that for clean configuration

Answer 4

lower

Question 5

Climbing at constant IAS and maximum climb thrust, the climb angle ___ and the pitch angle ___

Answer 5

decreases, decreases

Question 6

Vx and Vy ___ with increasing mass

Answer 6

increase