Interpretation of waverider performance data using computational fluid dynamics
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46616
Reference12 articles.
1. Optimized Scramjet Integration on a Waverider
2. Navier-Stokes computations of a viscous optimized waverider
3. Viscous optimized hypersonic waveriders designed from axisymmetric flow fields
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1. Design and Evaluation of a Hypersonic Waverider Vehicle Using DSMC;Computation;2024-07-09
2. Design exploration on the drag reduction and thermal protection over a blunted waverider with multiple opposing jets;Aerospace Science and Technology;2022-05
3. Study on Compression Surface Deformation of Waveriders;21st AIAA International Space Planes and Hypersonics Technologies Conference;2017-03-02
4. Numerical modeling of the flow conditions in a closed-circuit low-speed wind tunnel;Journal of Wind Engineering and Industrial Aerodynamics;2006-10
5. Experimental Results on a Mach 14 Waverider with Blunt Leading Edges;Journal of Aircraft;1997-05
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