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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Fundamentals Of Modern Unsteady Aerodynamics

ISBN: 9783030607760,9783030607777

3rd Edition

Authors: Ülgen Gülçat

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Question Posted: Apr 17, 2024 04:01 AM

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Find for a waverider flying at (80 mathrm{~km}) altitude with a Mach number of 25, find: (i)

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To find the approximate lifting pressure lift coefficient and induced drag coefficient for a waverid...View the full answer

Fundamentals Of Modern Unsteady Aerodynamics

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