When flaps are deployed on a wing they increase the on a large portion of ? [ Registration takeoff ]

Question 34-1 : Camber dihedral chord line aspect ratio

When flaps are deployed on a wing they increase the on a large portion of ?

Question 34-2 : Lift drag weight surface

When your fixed wing drone aircraft type makes a sharp turn it will ?

Question 34-3 : Cause the load factor to increase cause the stall speed to decrease cause horizontal control problems cause the load factor to decrease

Aircraft parts and components .from the tip to the hub of a propeller blade the ?

Question 34-4 : Increases changes according the speed decreases remains unchanged by definition

Aircraft parts and components .a propeller blade .1 has no preferential ?

Question 34-5 : 2 3 1 3 2 4 1 4

In order to increase the take off performance of your drone you will choose ?

Question 34-6 : Low pitch propellers high pitch propellers propellers dedicated to cruise flight reverse pitch propellers

On a multirotor remotely piloted aircraft the centering refers to the location ?

Question 34-7 : Longitudinal and lateral axis of the aircraft vertical axis of the aircraft lateral axis of the aircraft longitudinal axis of the aircraft

For a fixed wing drone vertical stabilizer assists in ?

Question 34-8 : Directional stability lateral stability longitudinal stability pitch control

For a fixed wing drone horizontal stabilizers assist in ?

Question 34-9 : Lateral stability longitudinal stability roll control directional stability

Principles of flight .around a wing cross section airflow speed is faster on ?

Question 34-10 : The upper surface the trailing edge the lower surface the leading edge

Principles of flight .two forms of airflow exist around a body ?

Question 34-11 : The laminar flow and the turbulent flow the vortex flow and the turbulent flow the turbulent flow and the regular flow the uniform flow and the tumultuous flow

Aerofoils .all other factors of importance remaining constant when speed is ?

Question 34-12 : Lift and drag increase lift increases and drag decreases lift decreases and drag increases lift and drag decrease

Aerofoils .at constant angle of attack for a fixed wing aircraft if speed is ?

Question 34-13 : Lift and drag decrease lift and drag increase lift decreases and drag increases lift increases and drag decreases

Aerofoils .at constant speed if angle of attack of a fixed wing airplane is ?

Question 34-14 : Lift increases until the critical angle of attack is exceed then lift decreases lift decreases until the critical angle of attack is exceed then lift increases lift decreases for all angles of attack lift increases for all angles of attack

Aerofoils .the angle between relative airflow and the chord line is ?

Question 34-15 : The angle of attack the pitch angle the descent path angle the climb path angle