FLIGHT FINAL Flashcards
(83 cards)
What are the two ways the coefficient of lift can be increased?
- increase AoA
- shape of wing
What is relative wind?
velocity and direction of airflow experienced by flying animal due to combined motion of their bodies through air and local wind direction
What two things does relative wind influence?
- velocity with which air flows past a flying animal’s wings
- angle of attack
What is profile drag?
pressure drag + friction drag
How is the total aerodynamic force determined?
determined by integrating the pressure acting across the entire wing surface
What are the two components of aerodynamic force?
- lift component (perpendicular to relative wind)
- drag component (parallel to relative wind)
What is the resultant?
sum of lift and drag components
What is thrust?
force moving propeller forward (parallel to oncoming fluid flow)
component of aerodynamic resultant directed forwards
What is force (torque) opposing blade motion?
resistance that engine needs to overcome to turn propeller (perpendicular to oncoming fluid flow)
What is pitch angle?
angle between longitudinal axis (where airfoil is pointed) and horizon
angle between chord of propeller blade and direction of rotation
How is pitch angle related to AoA?
changes to maintain AoA to relative wind
some pitch is selected to produce positive AoA to produce favourable L/D ratio and generate thrust
What is parasitic drag?
drag due to animal’s shape – combination of pressure drag, friction drag across body surface, and interference drag
What is interference drag?
drag caused by mixing of airflow components between wing and body
What is induced drag?
drag due to lift production
What is a ‘fictitious’ bound vortex equivalent to?
circulation around wing due to higher air speed over than under aerofoil
How is induced drag produced?
- downwash behind training edge of wing
- downwash causes relative wind to be pushed down at the trailing edge – magnitude of downwash and downward deflection is most pronounced close to wingtip, but occurs behind entire wing too
- effect relative wind acting on aerofoil now has slight downward deflection at an angle between angle of wind in downwash and oncoming relative wind
- lift remains perpendicular to effective relative wind, therefore it is tilted rearwards
- this backwards-tilted effective lift now directs more force rearwards – INDUCED DRAG
SUMMARY:
- wing and wingtip vortices produce downwash behind wing
- causes effective AoA of wing to decrease
- causes lift to be directed downstream = induced drag
At low flight velocities, is there low or high induced drag?
high
- at low airspeed, high CL produced by high AoA is needed to generate sufficient lift for flight
- downwash angle is increase compared to relative wind, tilting lift vector back towards trailing edge – high induced drag
At high flight velocities, is there low or high induced drag?
low
- low AoA is sufficient for lift
Is parasite drag low or high at low airspeed?
relatively low
Is parasite drag low or high at high airspeed?
relatively high – increases with v^2
Do wings with a low aspect ratio suffer less or more from induced drag?
more – due to the greater influence of the downwash behind the trailing edges of the wing
What are wings with low aspect ratio good for? Not good for?
- short wings good for rapid takeoff
- not good for extended flight
What are wings with medium aspect ratio good for?
- good for hovering
- slotted primary feathers reduce vorticity at wing tips
What are wings with high aspect ratio good for?
- increased lift relative to drag
- reduced induced drag
- gliding and soaring