Methods of Approximating Inviscid Jet Boundaries for Highly Underexpanded Supersonic Nozzles
Report Number: AEDC TDR 62-7 Author: Henson, J. R. Author: Robertson, J. E. Corporate Author: Arnold Engineering Development Center Laboratory: Arnold Engineering Development Center Date of Publication: 1962-05 Pages: 63 Contract: AF 40(600)-800 AD Number: AD0275641Contrails does not possess a copy of this report. Click here to offer Contrails a donation of this report
Abstract: 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.