Velocity field near a wing-fuselage combination at an angle of attack in a supersonic stream

DOI10.1007/BF01096643zbMath0468.76056OpenAlexW2045690557MaRDI QIDQ1156602

S. I. Kusakin

Publication date: 1980

Published in: Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf01096643

zbMATH Keywords

three-dimensionalvelocity fieldaerodynamic characteristics of aircraftarbitrarily profiledneighborhood of Mach conesingular term of the asymptotic expansionsupersonic edgeswing-fuselage combination at angle of attack

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Asymptotic approximations, asymptotic expansions (steepest descent, etc.) (41A60) Supersonic flows (76J20) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)

Cites Work

• On the determination of uniformly accurate solutions of differential equations by the method of perturbation of coordinates
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