When flaps are deployed on a wing they increase the on a large portion of the wing ?
Registration > takeoff
When flaps are deployed on a wing they increase the on a large portion of the wing ?
When your fixed wing drone aircraft type makes a sharp turn it will ?
Aircraft parts and components from tip to hub of a propeller blade angle of attack Increases, changes according speed, decreases, remains unchanged definition. 
Aircraft parts and components a propeller blade 1 has no preferential rotation direction2 has a rotation direction3 has an upper and a lower surfaces4 has no upper or lower surfacesthe combination regrouping all correct statements 
In order to increase take off performance of your drone you will choose Low pitch propellers, high pitch propellers, propellers dedicated to cruise flight, reverse pitch propellers. 
On a multirotor remotely piloted aircraft centering refers to location of center of gravity cg along Longitudinal lateral axis of aircraft, vertical axis of aircraft, lateral axis of aircraft, longitudinal axis of aircraft. Question Section 7: Theory of flight 34 Answer 8
For a fixed wing drone vertical stabilizer assists in Directional stability, lateral stability, longitudinal stability, pitch control. Question Section 7: Theory of flight 34 Answer 9
For a fixed wing drone horizontal stabilizers assist in Lateral stability, longitudinal stability, roll control, directional stability. Question Section 7: Theory of flight 34 Answer 10
Principles of flight around a wing cross section airflow speed faster on The upper surface, the trailing edge, the lower surface, the leading edge. Question Section 7: Theory of flight 34 Answer 11
Principles of flight two forms of airflow exist around a body The laminar flow the turbulent flow, the vortex flow the turbulent flow, the turbulent flow the regular flow, the uniform flow the tumultuous flow. Question Section 7: Theory of flight 34 Answer 12
Aerofoils all other factors of importance remaining constant when speed increased Lift drag increase, lift increases drag decreases, lift decreases drag increases, lift drag decrease. Question Section 7: Theory of flight 34 Answer 13
Aerofoils at constant angle of attack a fixed wing aircraft if speed decreased Lift drag decrease, lift drag increase, lift decreases drag increases, lift increases drag decreases. Question Section 7: Theory of flight 34 Answer 14
Aerofoils at constant speed if angle of attack of a fixed wing airplane increased Lift increases until critical angle of attack exceed, then lift decreases, lift decreases until critical angle of attack exceed, then lift increases, lift decreases all angles of attack, lift increases all angles of attack. Question Section 7: Theory of flight 34 Answer 15
Aerofoils the angle between relative airflow and chord line The angle of attack, the pitch angle, the descent path angle, the climb path angle.
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494 Free Training Exam Other source study: Codebateau examen 34