Compressible boundary-layer computation by the method of weighted residuals using exponentials.

12 Lapidus, A., "A Detached Shock Calculation by Second Order Finite Differences," Journal of Computational Physics, Vol. 2, 1967, pp. 154-177. 13 Moretti, G., "The Importance of Boundary Conditions in the Numerical Treatment of Hyperbolic Equations," PIBAL Kept. 68-34, 1968, Polytechnic Inst. of Brooklyn, New York. 14 Sheeran, W. J. and Dosanjh, D. S., "Investigations of Interacting Jet Flows, Part II: a) Single, Two-Dimensional, Underexpanded Jet Flows from a Sonic Nozzle, b) Interaction of Transversely Impinging, TwO-Dimensional Jet Flows," Rept. ME 1058-6608F, Aug. 1966, Syracuse University Research Inst., Dept. of Mechanical and Aerospace Engineering, Syracuse Univ., Syracuse, N. Y. 15 Sterrett) J. R. and Barber, J. B., "A Theoretical and Experimental Investigation of Secondary Jets in a Mach 6 Free Stream with JCmphasii§ on the Structure of the Jet and Separation Ahead of the Jet," Separated Flows, Part II, Proceedings of the AGARD Conference, NATO, No. 4, 1966, pp. 677-700.