Flow Simulation of Atmospheric Re-entry Vehicle at Varying Mach Number and Angle of Attack
Author:
Publisher
Springer Singapore
Link
http://link.springer.com/content/pdf/10.1007/978-981-15-5463-6_23
Reference21 articles.
1. Mehta RC (1996) Computations of flowfield over reentry modules at high speed
2. Kumar CN (2017) Computational flow analysis of apollo re-entry vehicle using 6(12):182–190
3. Kaushikh K, Arunvinthan S, Pillai SN (2018) Aerodynamics and aerothermodynamics of undulated re-entry vehicles. Acta Astronaut 142(17):95–102
4. Chen B, Zhan H, Zhou W (2015) Aerodynamic design of a re-entry capsule for high-speed manned re-entry. Acta Astronaut 106:160–169
5. Massimi HS, Shen H, Wen CY, Chen YS, Liang SM (2015) Numerical analysis of hypersonic flows around blunt-nosed models and a space vehicle. Aerosp Sci Technol 43:360–371
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