Date of Award

9-2009

Degree Name

MS in Mechanical Engineering

Department

Mechanical Engineering

Advisor

William Murray

Abstract

Compound aerospike nozzles were designed and tested as part of an ongoing

experimental study to determine the feasibility of thrust vectoring an aerospike

nozzle with the addition of a secondary port. Earlier phases of the study have

indicated that a compound aerospike nozzle could provide sufficient thrust

vectoring. The addition of a hole-type secondary port was found to provide

effective thrust vectoring.

Experiments were carried out to determine the effects of secondary port size,

secondary port inlet geometry and compound aerospike nozzle chamber

pressure. Results show good predictability, axisymmetric flow, and emphasize

the importance of a radius on secondary port inlet geometry.

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