Efficient Transonic Shock-Free Wing Redesign Procedure Using a Fictitious Gas Method

DOI10.2514/3.50744zbMath0417.76014OpenAlexW1998593580MaRDI QIDQ3208277

N. Jong Yu

Publication date: 1980

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.50744

zbMATH Keywords

full potential equationsupersonic regionfictitious gas methodcorrecting for viscous effectsOnera M6 planformtransonic shock-free wing redesign procedure

Mathematics Subject Classification ID

Supersonic flows (76J20) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)

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Computational methods for aerodynamic shape design

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