Numerical calculation of unsteady transonic potential flow over three-dimensional wings with oscillating control surfaces

DOI10.2514/3.8425zbMath0596.76072OpenAlexW2131499882MaRDI QIDQ3730240

Kohei Suetsugu, Koji Isogai

Publication date: 1984

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

Full work available at URL: https://doi.org/10.2514/3.8425

zbMATH Keywords

shock wavesangle of attackpressure distributionssupercritical flowsperturbation velocity potentialunsteady transonic potential flowsurface oscillationthree-dimensional oscillating wingsunsteady full potential equationunsteady transonic aerodynamic forces

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Transonic flows (76H05)

Related Items (1)

Geometric-control formulation and averaging analysis of the unsteady aerodynamics of a wing with oscillatory controls

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