Abstract
References 1 Chapman, D. R., An Analysis of Pressure at Supersonic Velocities and Comparison with Experiment, Rept. 1051, 1951, NACA. 2 Love, E. S., Base Pressure at Supersonic Speeds on TwoDimensional Airfoils and on Bodies of Revolution with and without Fins Having Turbulent Boundary Layers, TN 3819, Jan. 1957, NACA. 3 Whiffield, J. D. and Potter, J. L., On Pressures at High Reynolds Numbers and Hypersonic Mach Numbers, AEDC TN 60-61, March 1960, Arnold Engineering Development Center, Tullahoma, Tenn. 4 Potter, J. L., Whitfield, J. D., and Strike, W. T., Measurements and the Correlation of Transition Sensitive Data, AEDC TR 59-4, Feb. 1959, Arnold Engineering Development Center, Tullahoma, Tenn. 5 Cassanto, J. M., Base Pressure Results at M — 4 Using FreeFlight and Sting-Supported Models, AIAA Journal, Vol. 6, No. 7, July 1968, pp. 1411-1414. 6 Bogdonoff, S. M., A Preliminary Study of Reynolds Number Effects on Pressure at M = 2.95, Journal of Aeronautical Sciences, Vol. 19, No. 3, March 1952, pp. 201-206. 7 Kurzweg, H. H., Interrelationship Between Boundary Layer and Pressure, Journal of the Aeronautical Sciences, Vol. 18, No. 11, Nov. 1951, pp. 743-748. 8 Crocco, L. and Lees, L., A Mixing Theory for the Interaction Between Dissipative Flows and Nearly Isentropic Streams, Journal of the Aeronautical Sciences, Vol. 19, No. 10, Oct. 1952, pp. 649-676. 9 Cassanto, J. M., Radial Pressure Gradients in Laminar Flow, AIAA Journal, Vol. 5, No. 12, Dec. 1967, pp. 2278-2279. 10 Cassanto, J. M. and Hoyt, T. L., Flight Results Showing the of Mass Addition on Pressure, TIS 70SD248, March 1970, General Electric Company, Re-Entry and Environmental Systems Division, Philadelphia, Pa.; also AIAA Journal, Vol. 8, No. 9, Sept. 1970, pp. 1705-1707. 11 Cassanto, J. M., Effect of Cone Angle and Bluntness Ratio on Pressure, AIAA Journal, Vol. 3, No. 12, Dec. 1965, pp. 23512352. 12 Cassanto, J. M. and Storer, E. M., A Revised Technique for Predicting the Pressure of Sphere Cone Configurations in Turbulent Flow Including Mass Addition Effects, ALFM 68-41, Oct. 1968, General Electric Company, Re-Entry and Environmental Systems Division, Philadelphia, Pa. 13 Sherman, M. M., and Nakamura, T., Flight Test Measurements of Boundary Layer Transition on a Non-Ablating 22° Cone, Journal of Spacecraft and Rockets, Vol. 7, No. 2, Feb. 1970, pp. 137-142 14 Ames Research Staff, Equations, Tables, and Charts for Compressible Flow, Rept. 1135, 1953, NACA.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
