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Experimental investigation on aerospike nozzle in different structures and working conditions

  • Beihang University

Research output: Contribution to conferencePaperpeer-review

Abstract

For an approximate design of aerospike nozzle, some numerical and experimental studies and conclusions are given here. The numerical simulations contain of both the Method of Characteristic and the solving of the Navier-Stokes equations. The experimental system and several kinds of the test aerospike nozzle are showed here. Some tests and calculations curves are presented and explained.

Original languageEnglish
StatePublished - 2001
Event37th Joint Propulsion Conference and Exhibit 2001 - Salt Lake City, UT, United States
Duration: 8 Jul 200111 Jul 2001

Conference

Conference37th Joint Propulsion Conference and Exhibit 2001
Country/TerritoryUnited States
CitySalt Lake City, UT
Period8/07/0111/07/01

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