Analytical Modeling of Supersonic Retropropulsion Plume Structures
Author:
Affiliation:
1. Daniel Guggenheim School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, Georgia 30332
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.A32391
Reference12 articles.
1. McGheeR. 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.
2. JarvinenP. O.AdamsR. H. “The Aerodynamic Characteristics of Large Angled Cones with Retrorockets,” NASA CR NAS 7-576, Feb. 1970.
3. Supersonic Retropropulsion Experimental Results from the NASA Langley Unitary Plan Wind Tunnel
4. Analysis of Inviscid Simulations for the Study of Supersonic Retropropulsion
5. Comparison of Inviscid and Viscous Aerodynamic Predictions of Supersonic Retropropulsion Flowfields
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