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The use of transonic slender-body theory to calculate the spatial flow over a wing-fuselage configuration - MaRDI portal

The use of transonic slender-body theory to calculate the spatial flow over a wing-fuselage configuration

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Publication:1264660

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zbMath0913.76043MaRDI QIDQ1264660

V. V. Negoda, K. G. Sayadyan

Publication date: 25 May 1999

Published in: Computational Mathematics and Mathematical Physics (Search for Journal in Brave)

zbMATH Keywords

perturbed velocity potential function composite solution aerodynamic characteristics

Mathematics Subject Classification ID

Transonic flows (76H05) Finite difference methods applied to problems in fluid mechanics (76M20)

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