Maurice Tutor

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    Argosy University/ Phoniex University/
    Nov-2005 - Oct-2011

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    Phoniex University
    Oct-2001 - Nov-2016

Category > Management Posted 29 Apr 2018 My Price 3.00

unpowered flight

On its final approach to the airport, an airplane flies on a flight path that is 3.0° relative to the horizontal. What lift-to-drag ratio is needed if the airplane is to land with its engines idled back to zero power? (See Problem 9.112.)

Problem 9.112

Show that for unpowered flight (for which the lift, drag, and weight forces are in equilibrium) the glide slope angle, θ, is given by tan θ = CD/CL.

 

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Maurice Tutor
(5)
Status NEW Posted 29 Apr 2018 07:04 PM My Price 3.00

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