Configurations for High Supersonic Speeds Derived from Simple Shock-waves and Expansions
- 1 May 1963
- journal article
- research article
- Published by Cambridge University Press (CUP) in Journal of the Royal Aeronautical Society
- Vol. 67 (629) , 287-290
- https://doi.org/10.1017/s0368393100078597
Abstract
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.Keywords
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