Wall pressure fluctuations over a bulbous heat shield of a satellite launch vehicle

Author:

Mehta R. C.

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Computational Mechanics

Reference21 articles.

1. Bourgine, A.: Etude des fluctuations de pression pariétales, en écoulement transonique, sur ensemble cone-cylinder présentant un retreint. ONERA TP No 942, 1971.

2. Mehta, R. C.: Transonic flow simulation for a bulbous heat shield. J. Spacecraft Rockets34, 561?564 (1997).

3. Doerffer, P., Zierep, J.: An experimental investigation of the Reynolds number effect on a normal shock wave-turbulent boundary layer interaction on a curved wall. Acta Mech.73, 77?93 (1988).

4. Lighthill, M. J.: On sound generated aerodynamically. Proc. R. Soc. London Ser.A 211, 564?587 (1952).

5. hayden, R. E., Kadman, Y., Bliss, D. B., Afrik, S. A.: Diagnostic calculations of airframeradia noise. Prog. Astron. Aeron.45, 179?201 (1976).

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1. Numerical Flowfield Visualization Over Heat Shield Of Satellite Launch Vehicle at Mach 0.8 - 3.0;Journal of Aerospace Sciences and Technologies;2023-08-08

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4. Methods for Optimization of a Launch Vehicle for Pressure Fluctuation Levels and Drag;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05

5. Numerical study of flow field visualizations over a payload shroud at transonic speeds;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2008-12-19

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