Maurice Tutor

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Teaching Since: May 2017
Last Sign in: 398 Weeks Ago, 5 Days Ago
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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 29 Apr 2018 My Price 3.00

cruising speed

The wing area of a small airplane weighing
6.22 kN is 10.2 m2. (a) If the cruising speed of the plane is
210 kmhr, determine the lift coefficient of the wing. (b) If the
engine delivers 150 kW at this speed, and if 60% of this power
represents propeller loss and body resistance, what is the drag
coefficient of the wing.
(ANS: 0.292; 0.0483)

Answers

Maurice Tutor
(5)
Status NEW Posted 29 Apr 2018 09:04 PM My Price 3.00

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