Optimization of Supersonic Rocket Nozzles with Viscous Flow
The determination of the optimum shape of a supersonic (rocket motor) nozzle, under the constraint of a given surface area, while taking into account the effects of viscous action and heat conduction, is the objective of the investigation. In the case of a nozzle (low density or low Reynolds number)...
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| Format: | Book |
| Language: | English |
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Ft. Belvoir
Defense Technical Information Center
OCT 1970
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