Flight Flashcards
Aircraft Stability
The tendency of an aircraft in flight to remain in straight and level flight, and to return to this attitude if disturbed without corrective action from the pilot.
Static Stability
The initial tendency to return (initial ‘wave’ motion).
Dynamic Stability
Overall tendency to return (diminishing ‘wave’ motion
Inherent Stability
The stability of the airplane due to its in built features.
Angle of Attack
Angle between chord line and relative airflow.
Induced Drag
Created by lifting surfaces of aircraft, cannot be eliminated. Decreases as aircraft speed increases.
Parasite Drag. 3 types. How to reduce each.
Form Drag- created by frontal form or shape of aircraft body. Reduced by retractable landing gear, no wing struts, streamlining.
Skin Friction- resistance of aircraft body to move through air. Reduce by keeping aircraft free of dirt, polishing, flush rivets.
Interference Drag- created by the joining of 2 aircraft parts. Struts to fuselage, wing to fuselage.
All 3 increase as aircraft speed increases.
Lift explained by Newtons 3rd Law
Every action creates and equal and opposite reaction. Airflow is directed downwards by airfoil, creating the reaction of lift.
Lift explained by Bernoulli’s Principle
As a stream of fluids velocity increases, pressure decreases. An airfoil’s shape causes the airflow overtop of the wing to speed up, causing pressure to decrease. With more pressure underneath the wing, lift is created.
What are wing tip vortices. Explain ground effect.
Circular swirls of air created by an airfoil creating lift. Ground effect is when the aircraft is close to the ground, and created vortices are interrupted and the risk is minimized.
What are wing flaps
High lift devices which increase the camber of the airfoil and in some cases increases surface area of the wing.
What are the 3 axes of an aircraft. What is the name of movement that each one controls.
Longitudinal axis- nose to tail. Controls bank.
Lateral axis- wingtip to wingtip. Controls pitch.
Vertical axis- passes through center of aircraft as a vertical line. This movement is yaw.
Which three instruments are in the pitot-static system. What information does each one show. What does each use to receive the information.
Altimeter- Shows height (altitude). Static port takes in air to read pressure.
Airspeed indicator- Show airspeed using the pitot tube.
Vertical speed indicator- indicates speed of climb/decent. Measures rate of pressure change in static system.
What are the four strokes of an engine in order.
Induction, Compression, Ignition, Power
4 requirements to act as a flight crew member.
Appropriate (and valid) permit, license, rating, medical certificate. The pilot must be able to produce the documents.