Abstract
Received Dec. 10, 1975; synoptic received May 17, 1976. Full paper available from National Technical Information Service, Springfield, Va., 22151, as N-76-24154 at the standard price (available upon request). The author wishes to express his appreciation to his advisor, Earl Dowell, for his helpful advice and comments. Index categories: Subsonic and Transonic Flow; Nonsteady Aerodynamics. *Assistant-in-Research, Department of Aerospace and Mechanical Sciences. correction term. No empiricism beyond that inherent in an inviscid, potential flow model is involved. Comparisons with experimental and other theoretical data are encouraging and show that the method is reasonably accurate for shock-free flows.
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