Abstract
References 1 Darwell, H. M. and Trubridge, G. F. P., Design of Roclcet Nozzles to Reduce Gas Misalignment, Journal of Spacecraft and Rockets, Vol. 6, No. 1, Jan. 1968, pp. 36-41. 2 Ransom, V. H., Thompson, H. D., and Hoffman, J. D., A SecondOrder Bicharacteristics Method for Three-Dimensional, Steady Supersonic Flow, AIAA Journal, Vol. 10, No. 12, Dec. 1972, pp. 1573-1581. 3 Rao, G. V. R., Exhaust Nozzle Contour for Maximum Thrust, Jet Propulsion, Vol. 28, No. 6, June 1958, pp. 377-382. 4 Back, L. H., Cuffel, R. F., and Massier, P. F., Influence of Contraction Section Shape and Inlet Flow Direction on Supersoni'c Nozzle Flow and Performance, Journal of Spacecraft and Rockets, Vol. 9, No. 6, June 1972, pp. 420-427.
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