Engineering aerodynamic heating method for hypersonic flow
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23665
2. North Carolina State University, Raleigh, North Carolina 27695
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.26355
Reference25 articles.
1. Application of an upwind algorithm to the three-dimensional parabolized Navier-Stokes equations
2. Comparison of nonequilibrium viscous-shock-layer solutions with shuttle heating measurement
3. Inviscid Surface Streamlines and Heat Transfer on Shuttle-Type Configurations
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