Maurice Tutor

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Algebra,Applied Sciences,Biology,Calculus,Chemistry,Economics,English,Essay writing,Geography,Geology,Health & Medical,Physics,Science Hide all
Teaching Since: May 2017
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  • MCS,PHD
    Argosy University/ Phoniex University/
    Nov-2005 - Oct-2011

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  • Professor
    Phoniex University
    Oct-2001 - Nov-2016

Category > Management Posted 10 Oct 2017 My Price 6.00

airfoil properties

An airplane weighs 180 kN and has a wing area of 160 m2 and a mean chord of 4 m. The airfoil properties are given by Fig. 7.25. If the plane is designed to land at V0 =1.2Vstall, using a split flap set at 60°, (a) what is the proper landing speed in mi/h? (b) What power is required for takeoff at the same speed?

Answers

Maurice Tutor
(5)
Status NEW Posted 10 Oct 2017 02:10 PM My Price 6.00

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