New Method for Designing Shock-Free Transonic Configurations

DOI10.2514/3.61209zbMath0409.76051OpenAlexW3170178985MaRDI QIDQ4197522

No author found.

Publication date: 1979

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

Full work available at URL: http://hdl.handle.net/2060/19790006826

zbMATH Keywords

TransonicDesigningshock-Free

Mathematics Subject Classification ID

Transonic flows (76H05) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)

Related Items (6)

Planar and axially symmetric configurations which are circumvented with the maximum critical Mach number ⋮ Lift airfoils close to the airfoils in a flow with the maximum ``critical Mach numbers ⋮ Computation of subcritical compressible flows ⋮ Similarity of transonic flows with addition of heat and mass ⋮ Computational methods for aerodynamic shape design ⋮ Potential flow along a wavy wall and transonic controversy

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