Effect of the Adverse Pressure Gradient on Vortex Breakdown

of the Influence of the Turbulent Boundary Layer on the Pressure Distribution over a Rigid Two-Dimensional Wavy Wall, TN D-6477, Aug. 1971, NASA. 4 Lighthill, M. J., On Boundary Layers and Upstream Influence II. Supersonic Flows without Separation, Proceedings of the Royal Society, Vol. A217, 1953, pp. 478 and 504; see also Quarterly Journal of Mechanics, Vol. 3, 1950, p. 303. 5 Benjamin, T. B., Shearing Flow over a Wavy Boundary, Journal of Fluid Mechanics, Vol. 6, 1959, p. 161. 6 Miles, J. W., On Panel Flutter in the Presence of a Boundary Layer, Journal of Aerospace Sciences, Vol. 26, No. 2, Feb. 1959, pp. 81-93. 7 McClure, J. D., On Perturbed Boundary Layer Flows, Rept. 62-2, June 1962, M.I.T. Fluid Dynamic Research Lab., Cambridge, Mass. 8 Anderson, W. J. and Fung, Y. C, The Effect of an Idealized Boundary Layer on the Flutter of Cylindrical Shells in Supersonic Flow, GALCIT Structural Dynamics Rept. SM62-49, Dec. 1962, Graduate Aeronautical Lab., California Institute of Technology, Pasadena, Calif. 9 E. F. E., of the Pressure Distribution on Oscillating Panels in Low Supersonic Flow with Turbulent Boundary Layer, NASA CR-691, Feb. 1967, Georgia Institute of Technology, Atlanta, Ga. 10 Do well, E. H., Generalized Aerodynamic Forces on a Flexible Plate Undergoing Motion in a Shear Flow with an Application to Panel Flutter, AIAA Journal, Vol. 9, No. 5, May 1971, pp. 834-841. 11 Ventres, C. S., Transient Panel Motion in a Shear Flow, AMS Rept. 1062, Aug. 1972, Princeton Univ., Princeton, N.J. 12 Garrick, I. E. and Rubinow, S. I., Theoretical Study of Air Forces on an Oscillating or Steady Thin Wing in a Supersonic Main Stream, TN 1383, July 1947, NACA. 13 Yates, J. E., A Study of Panel Flutter with the Exact Method of Zeydel, NASA CR-1721, Dec. 1970, Aeronautical Research Associates of Princeton, Princeton, N.J. 14 Do well, E. H. and Ventres, C. S., Derivation of Aerodynamic Kernel Functions, AIAA Journal, Vol. 11, No. 11, Nov. 1973, pp. 1586-1588.