Shockwave Oscillations Over the Conical Heat Shield Region of a Typical Launch Vehicle at Mach 0.95

Author:

Murugan K. N.,Arunkumar T.,Prasath M.,Ganesan V. R.

Publisher

Springer Singapore

Reference7 articles.

1. Coe Charles F, Steady and fluctuating pressures at transonic speeds on two space-vehicle payload shapes. NASA TM X-503

2. Chevalier HL, Robertson JE, Pressures fluctuations resulting from an alternating flow separation and attachment at transonic speed. AEDC-TDR-63-204

3. Ramasamy MA, Rajendra G (1978) Experimental investigation of transonic flow past a blunt cone-cylinder. J Spacecraft Rockets 15:120123

4. Purohit SC (1986) Navier-stokes solution for a conical payload shroud. J Spacecraft Rockets 23:590–596

5. Kumar R, Viswanath PR, Prabhu A, Mean and fluctuating pressure field in boat-tail separated flows at transonic speeds. In: 39th AIAA aerospace sciences meeting and exhibit, AIAA 2001-0582

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