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Avit 323 Block 9 Lift Equation DD Exam 100% Correct $15.99
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Avit 323 Block 9 Lift Equation DD Exam 100% Correct

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Lift Equation - ANSWERSLift=CL((ov2)/295)S Coefficient of Lift - ANSWERSthe ratio between dynamic pressure and lift pressure; measures efficiency of the airfoil generating lift What does not change the coefficient of lift? - ANSWERSweight, CG, aircraft pitch attitude (AOA) or aircraft weight ...

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  • January 6, 2025
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  • Avit 323 Block 9 Lift Equation DD
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Avit 323 Block 9 Lift Equation DD Exam
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Lift Equation - ANSWERSLift=CL((ov2)/295)S

Coefficient of Lift - ANSWERSthe ratio between dynamic pressure and lift pressure;
measures efficiency of the airfoil generating lift

What does not change the coefficient of lift? - ANSWERSweight, CG, aircraft pitch
attitude (AOA) or aircraft weight

Where can you find the wing surface area? - ANSWERSPOH Section 1
Archer: 172 sq. ft.

desire to keep lateral control through stall - ANSWERStip stalls last and root stalls first

washout - ANSWERSthe tip section has a negative twist, leading edge points down

stall strips - ANSWERScauses flow to seperate below critial angle of attack

best for stall pattern - ANSWERS"hershey bar wing"

rectangular and elliptical wings - ANSWERSstall at root first

tapered wing - ANSWERSstalls at trailing center first
Cl(max) - ANSWERSthe angle of attack where any increase in AOA will result in
decreased lift (stall)

Cl decreases when - ANSWERScritical angle of attack is exceeded

static pressure flows hight to low is a - ANSWERSfavorable gradient

static pressure flows low to high is a - ANSWERSadverse gradient

turbulent flow has - ANSWERShigh velocity throughout layer



stagnation point - ANSWERSa point in a flow field where the local velocity of the fluid is
zero
laminar flow - ANSWERS-flow separates earlier
-more pressure drag
-less viscous drag

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