Numerical Study of Hypersonic Boundary Layer Receptivity Characteristics Due to Freestream Pulse Waves

Author:

Tang Xiaojun,Yu Juan,Hui Tianli,Yang Fenglong,Yu Wentao

Publisher

InTech

Reference25 articles.

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2. Aso S, Hayashi K, Mizoguchi M. A study on aerodynamic heating reduction due to opposing jet in hypersonic flow. AIAA Paper. 2002;2002:646

3. Hayashi K, Aso S, Tani Y. Numerical study on aerodynamic heating reduction by opposing jet. Memoirs of the Faculty of Engineering. 2006;66(1):39-54

4. Ma YB, Zhong XL. Boundary-layer receptivity of Mach 7.99 Flow over a blunt cone to free-stream acoustic waves. Journal of Fluid Mechanics. 2006;556:55-103

5. Boiko AV. Receptivity of a flat plate boundary layer to a free stream axial vortex. European Journal of Mechanics - B/Fluids. 2002;21:325-340

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