Numerical Simulation of Gas Injection Effect on Boundary Layer Instability for Space Vehicles

Author:

Egorov Ivan,Obraz Anton,Palchekovskaya Natalia,Fedorov Alexander

Publisher

Springer International Publishing

Reference15 articles.

1. Morkovin, M.V.: Critical evaluation of transition from laminar to turbulent shear layers with emphasis on hypersonically traveling bodies. Air Force Flight Dynamics Laboratory. Technical Report AFFDL-TR-68-149, DTIC citation AD-686178 (1969)

2. Scott, C.J., Anderson, G.E.: Boundary-layer transition with gas injection. J. Aerosp. Sci. 25, 791 (1958)

3. Pappas, C.C., Okuno: A. heat-transfer measurement for binary gas laminar boundary layers with high rates of injection. Ames Research Center. Technical Note TN-D-2473, NASA, Washington, D.C (1964)

4. Reda, D.C.: Review and synthesis of roughness-dominated transition correlations for reentry applications. J. Spacecr. Rockets 39, 161–167 (2002)

5. Schneider, S.: Hypersonic boundary-layer transition with ablation and blowing. J. Spacecr. Rockets 47, 225–237 (2010)

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