Corpus ID: 26841272

Design of a Small Scale Aerospike Nozzle and Associated Testing Infrastructure for Experimental Evaluation of Aerodynamic Thrust Vectoring

@inproceedings{Eilers2010DesignOA,
  title={Design of a Small Scale Aerospike Nozzle and Associated Testing Infrastructure for Experimental Evaluation of Aerodynamic Thrust Vectoring},
  author={Shannon D. Eilers and M. Wilson and S. Whitmore},
  year={2010}
}

• Shannon D. Eilers, M. Wilson, S. Whitmore
• Published 2010
• Computer Science

A system for cold ow testing of an aerospike nozzle has been developed in an e ort to examine the e ectiveness of aerodynamic thrust vectoring and truncated nozzle base bleed. These tests are designed to produce results that will support the design of a system for hot ow testing of the same technologies. Design of a nozzle suitable for testing with reasonable cold-gas mass ow rates and measureable forces and moments involved an extensive parametric study. Conceptual-level computational uid… Expand

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