Questions and Answers 100% Pass
thrust - ✔✔-must be generated to overcome the natural resistance of drag
-newton's third law
>"for every action there is an equal and opposite reaction"
unaccelerated - ✔✔means the airplane neither speeds up or slows down, but remains at
a constant velocity
accelerating - ✔✔if thrust is greater than drag, the speed would increase - as speed
increases so does drag - it will build until it equals the new drag and we will once again
be unaccelerated
deceleration - ✔✔initially drag is greater than thrust (speed), but as we slow drag
decreases until it reaches equilibrium with thrust
propellers: rotating airfoil - ✔✔subject to stalls, induced drag, and other troubles that
affect airfoils
thrust equation - ✔✔newton's second law of motion
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, f=ma
propeller driven airplanes - ✔✔large mass of air accelerated to relatively low final
velocity
propeller: thrust available - ✔✔-propeller is an airfoil
-not 100% efficient
-produces induced and parasite drag
-affected by airflow disturbed by other blade
increase in forward velocity - ✔✔-angle of attack of blade decreases
-thrust decreases
fixed pitch prop - ✔✔peak efficiency at one airspeed
constant speed prop - ✔✔-more blade settings
-greater range of efficiency
reciprocating aircraft engine - ✔✔-power producing machine
-fuel flow directly proportional to power output
Output Power of an Engine: PLANK - ✔✔P-indicated effective pressure (psi)
L-length of stroke in ft or fractions of ft
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