Methods of Approximating Inviscid Jet Boundaries for Highly Underexpanded Supersonic Nozzles

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Report Number: AEDC TDR 62-7
Author(s): Henson, J. R., Robertson, J. E.
Corporate Author(s): Arnold Engineering Development Center
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-05
Pages: 63
Contract: AF 40(600)-800
DoD Task:
Identifier: AD0275641

Methods of approximating inviscid boundaries of jets exhausting from axisymmetric supersonic nozzles into a quiescent atmosphere and moving streams have been developed. Jet shapes from two typical afterbody configurations were calculated for various flight conditions. Good agreement with available theoretical and experimental data was obtained. A step-by-step calculational procedure is given in the Appendix.

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