Investigation of computational flow field over a re-entry capsule at high speed

Author:

Rathnavel S.,Balaji K.,Kumar P.S.,Sathesh Raja,Sankaran K.

Publisher

Centre for Evaluation in Education and Science (CEON/CEES)

Subject

Mechanical Engineering,Mechanics of Materials

Reference10 articles.

1. Mehta, R.C.: Computations of flow field over Apollo and OREX reentry modules at high speed, Indian Journal of Engineering & Materials Sciences, Vol 15, pp. 459-466, 2008.;

2. Ralphin Rose, J. B., Saranya, P., Bibal Benifa, J. V.: Investigation of computational flow fields and aero acoustic characteristics over a re-entry command module, Journal of Aerospace Engineering, SAGE Publications, 2016.;

3. Mathews, R.N., Shafeeque, A.P.: Hypersonic flow analysis on an atmospheric re-entry module, International Journal of Engineering Research and General Science, Volume 3, Issue 5, 2015.;

4. Shiva Prasad, U., Srinivas, G.: Flow Simulation over Re-Entry Bodies at Supersonic & Hypersonic Speeds, International Journal of Engineering Research and Development, Volume 2, Issue 4, 2012.;

5. Shafeeque A P.: CFD analysis on an atmospheric re-entry module, International Research Journal of Engineering and Technology, Volume: 04 Issue: 01, 2017.;

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1. Computational Analysis of Re-entry Space Vehicle at Supersonic and Hypersonic Speed;Solutions for Maintenance Repair and Overhaul;2023-11-09

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