Numerical Analysis of Hypersonic Flow Past Blunt Bodies with Aerospikes-Reference-Cited by-同舟云学术

Numerical Analysis of Hypersonic Flow Past Blunt Bodies with Aerospikes

Published:2016-07 Issue:4 Volume:53 Page:669-677
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Sebastian Jiss J.¹,Suryan Abhilash¹,Kim Heuy Dong²

Affiliation:

1. College of Engineering, Trivandrum, Kerala 695016, India

2. Andong National University, Andong 760749, Republic of Korea

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A33414

Reference31 articles.

1. ShoemakerJ. M. “Aerodynamic Spike Flow Fields Computed to Select Optimum Configuration at Mach 2.5 with Experimental Validation,” AIAA Paper 1990-0414, Jan. 1990.

2. Spike-nosed projectiles - Computations and dual flow modes in supersonic flight

3. AlexanderS. R. “Results of Tests to Determine the Effect of a Conical Wind Shield on the Drag of a Bluff Body at Supersonic Speeds,” NACA RM L6K08a, Jan. 1947.

4. MoeckelW. E. “Flow Separation Ahead of a Blunt Axially Symmetric Body at Mach Numbers 1.76 to 2.10,” NACA RM E51125, 1951.

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