Abstract
1962; also U.S.S.R. Computational Center for Mathematics and Mathematical Physics, No. 5, Pergamon Press, New York, 1963. 18 Ovsiannikov, L. V., Gas Flow with Straight Transition Line, Prikladnaya Matematicheskaia Mekhanika, Vol. XIII, 1949; also TM 1295, May 1951, NACA. 19 Hopkins, D. F. and Hill, D. E., Effect of Small Radius of Curvature on Transonic Flow in Axisymmetric Nozzles, AIAA Journal, Vol. 4, No. 8, Aug. 1966, pp. 1337-1343. 20 Norton, D. J., Subsonic, Transonic, and Supersonic Nozzle Flow by the Inverse Technique, Journal of Spacecraft and Rockets, Vol. 9, No. 6, June 1972, pp. 457-459. 21 van Tuyl, A. H., Calculation of Nozzle Flows Using Pade Functions, AIAA Journal, Vol. 11, No. 4, April 1973, pp. 537-541. 22 Cohen, M. J. and Nimery, D. A., The Design of Axisymmetric Convergent Cones with Plane Sonic Outlets, Israel Journal of Technology, Vol. 10, No. 1-2, 1972, pp. 69-83.
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