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Exam (elaborations)

Avit 323 Block 10 Exam: Thrust UPDATED Exam Questions and CORRECT Answers

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Avit 323 Block 10 Exam: Thrust UPDATED Exam Questions and CORRECT Answers thrust - CORRECT ANSWER - -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 - CORRECT ANSWER - means the airplane neither speeds up or slows down, but remains at a constant velocity

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Institution
AVIT 323
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AVIT 323

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Uploaded on
January 19, 2025
Number of pages
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Written in
2024/2025
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Avit 323 Block 10 Exam: Thrust UPDATED
Exam Questions and CORRECT Answers
thrust - CORRECT ANSWER - -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 - CORRECT ANSWER - means the airplane neither speeds up or slows
down, but remains at a constant velocity


accelerating - CORRECT ANSWER - 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 - CORRECT ANSWER - initially drag is greater than thrust (speed), but as
we slow drag decreases until it reaches equilibrium with thrust


propellers: rotating airfoil - CORRECT ANSWER - subject to stalls, induced drag, and
other troubles that affect airfoils


thrust equation - CORRECT ANSWER - newton's second law of motion
f=ma


propeller driven airplanes - CORRECT ANSWER - large mass of air accelerated to
relatively low final velocity


propeller: thrust available - CORRECT ANSWER - -propeller is an airfoil
-not 100% efficient
-produces induced and parasite drag

, -affected by airflow disturbed by other blade


increase in forward velocity - CORRECT ANSWER - -angle of attack of blade decreases
-thrust decreases


fixed pitch prop - CORRECT ANSWER - peak efficiency at one airspeed



constant speed prop - CORRECT ANSWER - -more blade settings
-greater range of efficiency


reciprocating aircraft engine - CORRECT ANSWER - -power producing machine
-fuel flow directly proportional to power output


Output Power of an Engine: PLANK - CORRECT ANSWER - P-indicated effective
pressure (psi)
L-length of stroke in ft or fractions of ft
A-area of the cylinder (sq. in.)
N-number of power strokes per min
K-number of cylinders


non-geared, direct drive engine - CORRECT ANSWER - BHP = SHP



thrust horsepower - CORRECT ANSWER - power that is imparted by the propeller to the
air


Propeller efficiency - CORRECT ANSWER - always less than 100%



power = - CORRECT ANSWER - force x velocity

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