Find for a waverider flying at (80 mathrm{~km}) altitude with a Mach number of 25, find: (i)
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Find for a waverider flying at \(80 \mathrm{~km}\) altitude with a Mach number of 25, find:
(i) approximate lifting pressure,
(ii) lift coefficient, and induced drag coefficient. Assume ideal flow.
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Related Book For
Fundamentals Of Modern Unsteady Aerodynamics
ISBN: 9783030607760,9783030607777
3rd Edition
Authors: Ülgen Gülçat
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