Aerodynamic design of nozzles with uniform outflow for hypervelocity ground-test facilities
A method is proposed for the aerodynamic design of nozzles with uniform outflow for supersonic and hypersonic ground-test facilities. This method involves the coupling of an open-source Reynolds-averaged Navier–Stokes computational fluid dynamics solver, Eilmer, with the simplex optimization method...
| Main Authors: | , , , , , |
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| Format: | Journal article |
| Language: | English |
| Published: |
American Institute of Aeronautics and Astronautics
2018
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