Inviscid Surface Streamlines and Heat Transfer on Shuttle-Type Configurations
Author:
Affiliation:
1. North Carolina State University, Raleigh, N.C.
2. NASA Langley Research Center, Hampton, Va.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.61887
Reference21 articles.
1. A complete numerical technique for the calculation of three-dimensional inviscid supersonic flows
2. Comparison of characteristics and shock capturing methods with application to the space shuttle vehicle
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