For a supersonic flow under which condition the root pressure distribution of a thin wing can be
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For a supersonic flow under which condition the root pressure distribution of a thin wing can be determined with 2-D analysis. Why?
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Related Book For
Fundamentals Of Modern Unsteady Aerodynamics
ISBN: 9783030607760,9783030607777
3rd Edition
Authors: Ülgen Gülçat
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