Computational investigations into heat transfer over a double wedge in hypersonic flows

Author:

Expósito Diego,Rana Zeeshan A.ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference39 articles.

1. A numerical method for solving the Navier-Stokes equations with application to shock-boundary layer interactions;MacCormack,1975

2. Numerical solutions of supersonic and hypersonic laminar flows over a two-dimensional compression corner;Hung,1975

3. Shock wave-turbulent boundary layer interaction in hypersonic flow;Holden,1972

4. A validation study of four Navier-Stokes codes for high-speed flows;Rudy,1989

5. Newly identified principle for aerodynamic heating in hypersonic flows;Zhu;J. Fluid Mech.,2018

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