Similarity and Key Parameters of Retropropulsion Assisted Deceleration in Hypersonic Wind Tunnels-Reference-Cited by-同舟云学术

Similarity and Key Parameters of Retropropulsion Assisted Deceleration in Hypersonic Wind Tunnels

Published:2021-07 Issue:4 Volume:58 Page:984-996
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Gutsche Kevin¹,Marwege Ansgar¹,Gülhan Ali¹

Affiliation:

1. DLR, German Aerospace Center, 51147 Cologne, Germany

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.A34910

Reference20 articles.

1. Scaling and Similitude in Single Nozzle Supersonic Retropropulsion Aerodynamics Interference

2. JarvinenP. O.AdamsR. H. “The Aerodynamic Characteristics of Large Angled Cones with Retrorockets,” NASA CR-124720, Feb. 1970.

3. Mc GheeR. J. “Effects of a Retronozzle Located at the Apex of a 140 deg Blunt Cone at Mach Numbers of 3.00, 4.50, and 6.00,” NASA TN-D-6002, Jan. 1971.

4. Dynamics of Shock Dispersion and Interactions in Supersonic Freestreams with Counterflowing Jets

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