Computational inlet-fairing effects and plume characterization on a hypersonic powered model
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681-0001
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46870
Reference11 articles.
1. Development and application of GASP 2.0
2. Hypersonic parabolized Navier-Stokes code validation on a sharp nosecone
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1. References;Aircraft Design: A Conceptual Approach, Seventh Edition;2024-08-15
2. Effect of Integration of Scramjet into Airframe on Engine Performance and Payload;Journal of Propulsion and Power;2002-09
3. Effect of Sides-Spillage from Airframe on Scramjet Engine Performance;Journal of Propulsion and Power;2001-01
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