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Configurations for High Supersonic Speeds Derived from Simple Shock-waves and Expansions
Published online by Cambridge University Press: 04 July 2016
Summary
The Nonweiler method of designing delta wings (caret wings) to have plane shocks on the lower surface is extended to the design of upper surfaces. Cambered and shock-free surfaces are also deduced, and methods of design for complete configurations suggested.
An important point is that all surfaces are of single curvature.
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- Copyright © Royal Aeronautical Society 1963
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