Lifting and nonlifting kernel functions for cascade and isolated airfoils

Abstract

References 1 East, R. A., Qasrawi, A. M., and Khalid, M., An Experimental Study of the Stability of Pitching Blunt Conical and Hyperballistic Shapes in a Short Running Time Facility, AGARD Conference Proceedings, No. 235, Nov. 1978. Khalid, M. and East, R. A., ''Stability Derivatives of Blunt Slender Cones at High Mach Numbers, Aeronautical Quarterly, Vol. 30, Nov. 1979, pp. 559-590. Eggers, A. J. and Savin, R. C., A Unified Two-Dimensional Approach to the Calculation of Three-Dimensional Flows with Application to Bodies of Revolution, NACA Rept. 1249, 1955. Stone, A. H., On Supersonic Flow Past a Slightly Yawing Cone, II, Journal of Math & Physics, Vol. 30, 1951, pp. 200-213. Kopal, Z., Tables of Supersonic Flow around Cones at Large Yaw, M.I.T. TR. No. 5, 1949. Taylor, G. I. and Maccoll, J. W., Air Pressure on a Cone Moving at High Speeds, Proceedings of the Royal Society of London, Series A, Vol. 139, Feb. 1933, pp. 278-311. Khalid, M., A Theoretical and Experimental Study of the Stability of Blunt Axisymmetric Conical and Power Law Shapes, Ph.D. Thesis, University of Southampton, Hants, England, 1977. Schueler, C. J., Dynamic Stability Results for a 10 deg Cone at Mach Numbers 0.8 to 20, AEDC-TDR 64-226, Dec. 1964. Marshall, L. A., Hypersonic Stability Summary, Pt. 1, Tech. Rept. AFFDL-TDR 66-149, Jan. 1967. Qasrawi, A. M., Unpublished data, University of Southampton, Hants, England, 1978. Ericsson, L. E., Effect of Nose Bluntness, Angle of Attack, and Oscillation Amplitude on Unsteady Aerodynamics of Slender Cones, AIAA Journal, Vol. 9, Feb. 1971, pp. 297-304.