Application of slender body theory to the calculation of aerodynamic properties of low aspect ratio wings with nacelles at their tips

DOI10.1016/0021-8928(58)90091-1zbMath0088.18802OpenAlexW2039005141MaRDI QIDQ3261146

V. V. Keldysh

Publication date: 1958

Published in: Journal of Applied Mathematics and Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0021-8928(58)90091-1

zbMATH Keywords

fluid mechanics

Cites Work

• SUPERSONIC FLOW PAST SLENDER POINTED BODIES

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