Abstract
On the basis of the present analysis of specific two and highly swept three-dimensional shock wave and turbulent boundary layer interactions, it has been observed that: 1) three-dimensional flows are radically different than the “classical” two-dimensional flows, 2) the scale, pressure gradients, unsteadiness, and computability are quite different, 3) the designation of “separation” in three dimensions is not realistic, and 4) a concept of vorticity rearrangement is proposed to describe the physics of the interactions in three dimensions.
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References
Green, J.E.: Interactions Between Shock Waves and Turbulent Boundary Layers. Progress in Aerospace Sciences, Vol. 11, 1970. D Kuchemann edt.
Peake, D.J.; Tobak, M.: Three-Dimensional Interactions and Vortical Flows with Emphasis on High Speeds. NASA TM 81169, 1980.
Settles, G.S.; Dolling, D.S.: Swept Shock Wave/Boundary-Layer Interactions. Tactical Missile Aerodynamics Volume, AIAA Progress in Astronautics and Aeronautics Series, M. Hemsch and J. Nielsen, eds. To be published 1986/87.
Settles, G.S.; Fitzpatrick, T.J.; Bogdonoff, S.M.: Detailed Study of Attached and Separated Compression Corner Flowfields in High Reynolds Number Supersonic Flow. AIAA Journal, Vol. 17, No. 6, June 1979.
Smits, A.J.; Hayakawa, K.; Bogdonoff, S.M.: Turbulence Measurements in Two Shock-Wave/Shear-Layer Interactions. Presented at the I.U.T. A.M. Symposium on the Structure of Complex Turbulent Shear Flow, Marseille, 1982. Published by Springer-Verlag.
Settles, G.S.; Bogdonoff, Seymour M.; Vas, Irwin E.: Incipient Separation of a Supersonic Turbulent Boundary Layer at High Reynolds Numbers. AIAA Journal, Vol. 14, No. 1, January 1976.
Settles, G.S: An Experimental Study of Compressible Turbulent Boundary Layer Separation at High Reynolds Numbers. Ph. D. Dissertation, Princeton University, September 1976.
Dolling, D.S.; Murphy, M.T.: Unsteadiness of the Separation Shock Wave Structure in a Supersonic Compression Ramp Flowfield. AIAA Journal, Vol. 21, No. 12, December 1983.
Muck, K.C.; Dussauge, Jean-Paul; Bogdonoff, S. M.: Structure of the Wall Pressure Fluctuations in a Shock--Induced Separated Turbulent Flow. AIAA Paper No. 85–0179, January 1985.
Shapey, B.: Three-Dimensional Shock Wave Turbulent Boundary Layer Interaction for a 20° Sharp Fin at Mach 3. MSE Thesis, Princeton University, Oct. 1986, in preparation.
Tan, D.K.M.; Tran, T.T.; Bogdonoff, S.M.: Surface Pressure Fluctuations in a Three-Dimensional Shock Wave Turbulent Boundary Layer Interaction. AIAA Paper 85–0125, January 1985.
Tran, T.T.; Tan, D.K.M.; Bogdonoff, S.M.: Surface Pressure Fluctuations in a Three-Dimensional Shock Wave/Turbulent Boundary Layer Interaction at Various Shock Strengths. AIAA Paper 85–1562, July 1985.
Tran, T.T.: Experimental Investigation of Unsteadiness in Swept Shock Wave/Turbulent Boundary Layer Interactions. Ph.D. Thesis, Princeton University, October 1986, in preparation.
Gramann, R.A.; Dolling D.S.: Unsteady Separation in Shock Wave Turbulent Boundary Layer Interaction. AIAA Paper No. 86–1033, May 1986.
Chapman, D.R.; Kuehn, D.M.; Larson, H.K.: Investigation of Separated Flows in Supersonic Stream with Emphasis on the Effect of Transition. NACA Rept. 1356, 1958.
Zheltovodov, A.A.: Regimes and Properties of Three-Dimensional Separation Flows Initiated by Skewed Compression Shocks. Zhurnal Prikladnoi Mekhaniki i Tekhnicheskoi Fiziki, No. 3, May-June 1982.
Korkegi, R.H.: A Lower Bound for Three-Dimensional Turbulent Separation in Supersonic Flow. AIAA Journal, Vol. 23, No. 3, March 1985.
Knight, D.; Horstman, C.; Shapey, B.; Bogdonoff, S.M.: The Flowfield Structure of the 3-D Shock Wave-Boundary Layer Interaction Generated by a 20 deg Sharp Fin at Mach 3. AIAA Paper No. 86–0343, January 1986.
Maskell, E.C.: Flow Separation in Three Dimensions. R.A.E. Rept. Aero. No. 2565, 1955.
Lighthill, M.J.: Attachment and Separation in Three-Dimensional Flow. In Laminar Boundary Layers, Oxford University Press, 1963.
Dallman, U.: Structural Stability of Three-Dimensional Vortex Flows. Nonlinear Dynamics of Transcritical Flows, edited by Jordaon, H. L., Oretel, H., and Robert, K., Springer-Verlag, Berlin, 1984.
Chapman, Gary T.: Topological Classification of Flow Separation on Three-Dimensional Bodies. AIAA Paper No. 86–0485, January 1986.
Inger, G.: Private communication, January 1986.
Lu, F.K.; Settles, G.S.: Conical Similarity of Shock/Boundary Layer Interactions Generated by Swept Fins. AIAA Journal, Vol. 83, No. 7, July 1985.
Oskam, B.: Three-Dimensional Flow Fields Generated by the Interaction of a Swept Shock Wave with a Turbulent Boundary Layer. Ph.D. Dissertation, Princeton University, September 1976.
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Bogdonoff, S.M. (1987). Observation of Three-dimensional “Separation” in Shock Wave Turbulent Boundary Layer Interactions. In: Smith, F.T., Brown, S.N. (eds) Boundary-Layer Separation. International Union of Theoretical and Applied Mechanics. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-83000-6_3
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DOI: https://doi.org/10.1007/978-3-642-83000-6_3
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