Aerodynamic design of axisymmetric hypersonic wind-tunnel nozzles using a least-squares/parabolized Navier-Stokes procedure
- 1 September 1992
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 29 (5), 685-691
- https://doi.org/10.2514/3.11511
Abstract
No abstract availableKeywords
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- Aerodynamic design of axisymmetric hypersonic wind-tunnel nozzlesJournal of Spacecraft and Rockets, 1970
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