The part of the wing shown by the arrow is 55 ? Preparation > drone
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Spoiler extension for a fixed wing drone causes ?
2 Spoiler extension a fixed wing drone causes An increase in drag decrease in lift.
Induced drag is associated with ?
3 Induced drag associated with An increase in drag decrease in lift. 4 Parasit drag associated with The friction of relative airflow on contour of aircraft. 5 Wing stall occurs when we exceed Its critical angle of attack. 6 When flaps are deployed on a wing they increase on a large portion of wing Its critical angle of attack. 7 When flaps are deployed on a wing they increase on a large portion of wing Its critical angle of attack. 8 When your fixed wing drone aircraft type makes a sharp turn it will Cause load factor to increase. 9 Aircraft parts and components from tip to hub of a propeller blade angle of attack Cause load factor to increase. 10 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 Cause load factor to increase. 11 In order to increase take off performance of your drone you will choose Low pitch propellers. 12 On a multirotor remotely piloted aircraft centering refers to location of center of gravity cg along Longitudinal lateral axis of aircraft. 13 For a fixed wing drone vertical stabilizer assists in Directional stability. 14 For a fixed wing drone horizontal stabilizers assist in Directional stability. 15 Principles of flight around a wing cross section airflow speed faster on Directional stability. 16 Principles of flight two forms of airflow exist around a body The laminar flow the turbulent flow. 17 Aerofoils all other factors of importance remaining constant when speed increased The laminar flow the turbulent flow. 18 Aerofoils at constant angle of attack a fixed wing aircraft if speed decreased The laminar flow the turbulent flow. 19 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. 20 Aerofoils the angle between relative airflow and chord line Lift increases until critical angle of attack exceed then lift decreases. Exclusive rights reserved. Reproduction prohibited under penalty of prosecution.
