Numerical Simulation of Entrainment and Recirculating flow at the Base of a Truncated Aerospike Nozzle with Supplementary Base Flow
abstract: The aerospike nozzle belongs to the class of altitude compensating nozzles making it a strong candidate for Space Shuttle Main Engines. Owing to their higher efficiency compared to conventional bell nozzles, the aerospike nozzles are being studied extensively and are being used for many Si...
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| Format: | Dissertation |
| Language: | English |
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2017
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| Online Access: | http://hdl.handle.net/2286/R.I.45499 |