3241.CQ4 - accelerations constant density(1 –u 2 ρ A)sin...

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3241: Aerodynamics and Flight Mechanics Name: _________________ Concept Quiz #4 The purpose of this concept quiz is to examine the application momentum equation for part of a control surface analysis. The momentum equation is: ( 29 = + F dS n U U dV U dt d S V d d d d ˆ ρ ρ What is the y-component of momentum flux across this surface? Assume steady flow, no
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Unformatted text preview: accelerations, constant density. (1) –u 2 ( ρ A)sin( θ )sin( θ ) (2) u 2 ( ρ A)sin( θ )sin( θ ) (3) –u 2 ( ρ A)cos( θ )cos( θ ) (4) u 2 ( ρ A)cos( θ )cos( θ ) (5) –u 2 ( ρ A)sin( θ )cos( θ ) (6) u 2 ( ρ A)sin( θ )cos( θ ) (7) I have no idea how to do this x U θ n A ρ y...
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