High-Enthalpy Aerothermodynamics of a Mars Entry Vehicle Part 2: Computational Results-Reference-Cited by-同舟云学术

High-Enthalpy Aerothermodynamics of a Mars Entry Vehicle Part 2: Computational Results

Published:1997-07 Issue:4 Volume:34 Page:457-463
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Hollis Brian R.¹,Perkins John N.¹

Affiliation:

1. North Carolina State University, Raleigh, North Carolina 27695-7910

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/2.3258

Reference24 articles.

1. High-enthalpy and perfect-gas heating measurements on a blunt cone

2. 4Hollis, B. R. “Experimental and Computational Aerothermodynamics of a Mars Entry Vehicle,” Ph.D. Dissertation, Dept. of Mechanical and Aerospace Engineering,NorthCarolina State Univ., Raleigh, NC,Dec. 1996; also NASA CR 201633, Dec. 1996.

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