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Flowfield Modeling of a Three-Dimensional Shock Wave Turbulent Boundary Layer Interaction

  • Conference paper
Separated Flows and Jets

Abstract

Modeling of the flowfield generated by the interaction of a shock wave and a turbulent boundary layer was carried out by using elements of a series of experiments and computations. Combining surface observations, flowfield surveys, and extensive computations, a model of the flowfield was derived. The key physical characteristics and parameters are discussed, along with the missing elements needed to further refine the model. The proposed model differs considerably from that of previous investigators. It gives a new view of the total flowfield structure and shows the inadequacy of using surface visualization as the basis for constructing the flowfield model.

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References

  1. Knight, D.; Horstman, C. C.; Ruderich, R.; Mao, M. F; Bogdonoff, S. M.: Supersonic turbulent flow past a 3-D swept compression corner at Mach 3. AIAA Paper #87–0551, January 1987.

    Google Scholar 

  2. Green, J. E.: Interactions between shock waves and turbulent boundary layers. Prop, in Aerospace Sciences. Vol. 11, 1970, ed. D. Kuchemann.

    Google Scholar 

  3. Settles, G. S.; Dolling, D. S.: Swept shock wave boundary-layer interactions. Review prepared for AIAA Progress in Astronautics and Aeronautics. Vol. 104 “Tactical Missile Aerodynamics”, Sept. 1986.

    Google Scholar 

  4. Settles, G. S.; Dolling, D. S.: Swept shock/boundary-layer interactions - tutorial and update. AIAA Paper #90–0375, January 1990.

    Google Scholar 

  5. Stalker, R. J.: Sweepback effects in turbulent boundary layer shock wave interaction. J. Aero/Space Sci.. 27. No. 5, 348 - 56, 1960.

    MathSciNet  MATH  Google Scholar 

  6. Stanbrook, A.: An experimental study of the glancing interaction between a shock wave and a turbulent boundary layer. RAE TN Aero 2701, ARC CP555, 1960.

    Google Scholar 

  7. Johnston, J. P.: On the three-dimensional turbulent boundary layer generated by secondary flow. J. Basic Eng. Series D, Trans. ASME 82, 233, 1960.

    Article  Google Scholar 

  8. Lowrie, B. W.: Cross-flows produced by the interaction of a swept Shockwave with a turbulent boundary layer. Ph.D. Thesis, Cambridge University, 1965.

    Google Scholar 

  9. McCabe, A.: The three-dimensional interaction of a shock wave with a turbulent boundary layer. Aero Quart. 17. 231–52, 1966.

    Google Scholar 

  10. Maskell, E. C.: Flow separation in three dimensions. RAE Rept. Aero. No. 2565, 1955.

    Google Scholar 

  11. Lighthill, M. J.: Attachment and separation in three-dimensional flow. In Laminar Boundary Layers. Oxford University Press, 1963.

    Google Scholar 

  12. Korkegi, R. H.: A lower bound for three-dimensional turbulent separation in supersonic flow. AIAA J.. Vol. 23, No. 3, March 1985.

    Google Scholar 

  13. Token, K. H.: Heat transfer due to shock wave/turbulent boundary layer interactions on high speed weapon systems. AFFDL TR-74–77, 1974.

    Google Scholar 

  14. Neumann, R. D.; Token, K. H.: Prediction of surface phenomena induced by three-dimensional interactions on planar turbulent boundary layers. Int. Astro. Fed. 25th Congr.. Paper No. 74–058.

    Google Scholar 

  15. Neumann, R. D.; Hays, J. R.: Prediction techniques for the character¬istics of the 3-D shock wave turbulent boundary layer interactions. AIAA JL, 15, 1469–1473, 1977.

    Article  ADS  Google Scholar 

  16. Hays, J. R.: Prediction techniques for the characteristics of fin generated three-dimensional shock wave/turbulent boundary layer interacion. AFFDL TR-77–10, 1977.

    Google Scholar 

  17. Kubota, H.; Stollery, J. L.: An experimental study of the interaction between a glancing shock wave and a turbulent boundary layer. J. Fluid Mech.. Vol. 116, pp. 431–458, 1982.

    Article  ADS  Google Scholar 

  18. Oskam, B.: Three-dimensional flowfields generated by the interaction of a swept shock wave with a turbulent boundary layer.. Ph.D. Thesis, Princeton University, September 1976.

    Google Scholar 

  19. Oskam, B.: Mach 3 oblique shock wave/turbulent boundary layer interactions in three dimensions. AIAA Paper No. 76–336, July 1976.

    Google Scholar 

  20. Goodwin, S. P.: An exploratory investigation of sharp fin-induced shock wave/turbulent boundary layer interactions at high shock strengths. MSE Thesis, Princeton University, December 1983.

    Google Scholar 

  21. Shapey, B. L.: 3-D shock wave/turbulent boundary layer interaction for a 20° sharp fin at Mach 3. MSE Thesis, Princeton University, October 1986.

    Google Scholar 

  22. Shapey, B. L.; Bogdonoff, S. M.,: Three-dimensional shock wave/turbulent boundary layer interaction for a 20° sharp fin at Mach 3. AIAA Paper No. 87–0554, January 1987.

    Google Scholar 

  23. Ketchum, A. C.: Analysis of the flowfield structure of several three- dimensional shock wave-boundary layer interactions from detailed static pressure measurements. MSE Thesis, Princeton University, November 1988.

    Google Scholar 

  24. a) Kimmel, R.; Bogdonoff, S.: A comparative experimental investigation of shock/turbulent boundary layer interactions produced by three shock generators. AIAA Paper #87–1366, June 1987.

    Google Scholar 

  25. b) Kimmel, R.: An experimental investigation of quasi-conical shock wave/turbulent boundary layer interactions. Ph.D. Dissertation, Princeton University, April 1987.

    Google Scholar 

  26. Kim, K.-S.; Lee, Y.; Alvi, F. S.; Settles, G. S.; Horstman, C. C.: Laser Skin Friction Measurements and CFD Comparison of Weak-to-Strong Swept Shock/Boundary-Layer Interactions. AIAA Paper #90-0378, January 1990.

    Google Scholar 

  27. Alvi, F. S.; Settles, G. S.: Structure of swept shock wave/boundary- layer interactions using conical shadowgraphy. AIAA Paper #90–1644, June 1990.

    Google Scholar 

  28. Settles, G. S.: An experimental study of compressible turbulent boundary layer separation at high Reynolds numbers. Ph.D. Thesis, Princeton University, September 1975.

    Google Scholar 

  29. Chapman, Gary T.: Topological classification of flow separation on three-dimensional bodies. AIAA Paper No. 86–0485, January 1986.

    Google Scholar 

  30. Zheltovodov, A. A.: Regimes and properties of three-dimensional separation flows initiated by skewed compression shocks. Zhurnal Prikladnoi Mekhaniki i Technicheskoi Fiziki, No. 3, May–June 1982.

    Google Scholar 

  31. Wang, S. Y.; Bogdonoff, S. M.: A re-examination of the upstream influence scaling and similarity laws for 3-D shock wave/turbulent boundary layer interaction. AIAA Paper No. 86 - 0347, January 1986.

    Google Scholar 

  32. Tran, T. T.: An experimental investigation of unsteadiness in swept shock wave/turbulent boundary layer interactions. Ph.D. Thesis, Princeton University, April 1987.

    Google Scholar 

  33. Tran, T. T.; Bogdonoff, S. M.: A study of unsteadiness of shock wave/turbulent boundary layer interactions from fluctuating wall pressure measurements. AIAA Paper No. 87 - 0552, January 1987.

    Google Scholar 

  34. Knight, D.; Horstman, C.; Shapey, B.; Bogdonoff, S.: The flowfield structure of the 3-D shock wave - boundary layer interaction generated by a 20° sharp fin at Mach 3. AIAA Paper No. 86 - 0343, January 1986.

    Google Scholar 

  35. Narayanswami, N.; Knight, D. D.: Viscous/inviscid effects in 3-D shock wave-turbulent boundary layer interactions. AIAA Paper No. 89–0358, January 1989.

    Google Scholar 

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Author information

Authors and Affiliations

  1. Gas Dynamics Laboratory, Princeton University, Princeton, NJ, USA

    Seymour M. Bogdonoff

  2. Mechanical and Aerospace Engineering Department, Princeton University, Princeton, NJ, USA

    Seymour M. Bogdonoff

Authors
  1. Seymour M. Bogdonoff
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Editor information

Editors and Affiliations

  1. Inst. of Theoretical & Applied Mechanics, Siberian Branch of the USSR Academy of Sciences, 630090, Novosibirsk, USSR

    V. V. Kozlov  & A. V. Dovgal  & 

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© 1991 Springer-Verlag, Berlin Heidelberg

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Bogdonoff, S.M. (1991). Flowfield Modeling of a Three-Dimensional Shock Wave Turbulent Boundary Layer Interaction. In: Kozlov, V.V., Dovgal, A.V. (eds) Separated Flows and Jets. International Union of Theoretical and Applied Mechanics. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-84447-8_38

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  • DOI: https://doi.org/10.1007/978-3-642-84447-8_38

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-84449-2

  • Online ISBN: 978-3-642-84447-8

  • eBook Packages: Springer Book Archive

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