Shock-wave-turbulent-boundary-layer interaction and its control: A survey of recent developments

Ackeret J, Feldman F, Rott N 1946 Investigations of compressior shocks and boundary layers in gases moving at high speed.NACA TM 1113

Adamson T C, Feo A 1975SIAM J. Appl. Math. 29: 121–145

Adamson T C, Messiter A F 1980Annu. Rev. Fluid Mech. 12: 103–138

Anyiwo J C, Bushnell D M 1982AIAA J. 20: 893–899

Bachalo W D, Johnson D A 1979 An investigation of transonic turbulent boundary layer separation generated on an axisymmetric flow model.AIAA Paper 79-1479

Bahi L, Ross J M, Nagamatsu H T 1983 Passive shock-wave/boundary layer interaction control for transonic airfoil drag reduction.AIAA Paper 83-037

Ball K O W 1970AIAA J. 8: 374–375

Ball K O W, Korkegi R H 1968AIAA J. 6: 239–243

Beam R M, Warming R F 1978AIAA J. 16: 393–402

Bradshaw P, Ferris D H, Atwell N P 1967J. Fluid Mech. 28: 593–616

Brusseleers M 1980Shock-boundary layer interactions in turbomachines, Von Karman Inst. (Belgium). Lecture Series 1980–8

Burggraf O R 1975 Flow separation,AGARD-CP-168, Paper no 10

Burggraf O R, Rizetta D, Werle M J, Vatsa V N 1979AIAA J. 17: 336–343

Carter J E 1975 Inverse solutions for laminar boundary layer flows with separation and reattachment,NASA TR-R-447

Cebcci T, Meier H U 1979 Turbulent boundary layers, experiments, theory and modelling.AGARD-CP-271

Cebeci T, Stewartson K, Whitelaw J H 1984Numerical and physical aspects of aerodynamic flows II (Berlin: Springer Verlag)

Chang P K 1976Control of flow separation (New York: Hemisphere)

Chapman D R, Kuehn D M, Larson H K 1957 Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition,NACA TN 3869

Charwat A F 1970Advances in heat transfer (eds) J P Hartnett, T F Irvine (New York: Academic Press) 6: 1–132

Chinneck A, Jones G C A, Tracey C M 1955 An interim report on the use of blowing to reduce fall in control effectiveness associated with shock-induced separation at transonic speeds,ARC 1756FM 2231

Coe C F, Chyu W J, Dods J B 1973 Pressure fluctuations underlying attached and separated supersonic turbulent boundary layers and shock waves,AIAA Paper 73-996

Crawford D H 1961 The effect of air bleed on heat transfer and pressure distribution on 30° flares at a Mach number of 6–8,NASA TMX-439

Crocco L, Lees L 1952J. Aero. Sci. 19: 649–676

Delery J M 1981 Investigation of strong shock-turbulent boundary layer interaction in 2-D transonic flows with emphasis on turbulence phenomena,AIAA Paper 81-1245

Delery J M 1983AIAA J. 21: 180–185

Delery J M 1985Prog. Aerosp. Sci. 22: 209–280

Dolling D S 1982AIAA J. 20: 1385–1391

Dolling D S, Murphy M T 1983AIAA J. 21: 1628–1634

Dolling D S, Or C T 1983 Unsteadiness of shock-wave structure in attached and separated compression corner ramp flow fields,AIAA Paper 83-1715

Don Gray J, Maus J R 1981AIAA J. 19: 948–950

Driver D M, Lee Seegmiller H, Marvin J G 1983 Unsteady behaviour of a reattaching shear layer,AIAA Paper 83-1712

Eaton J K, Johnston J P 1982Turbulent shear flows. 3. (eds) L J S Bradbury, F Durst, B E Launder, F W Schmidt, J H Whitelaw (Berlin: Springer Verlag)

Elfstrom G M 1972J. Fluid Mech. 53: 113–127

Erdos J, Pallone A 1962Proc. Heat Transfer & Fluid Mech. Inst. (Stanford: University Press)

Finke K 1975 Flow separation,AGARD-CP-168, Paper no. 28

Fukuda M K, Hingst W R, Reshotko E 1977AIAA J. 14: 151–156

Gadd G E 1961 Interactions between normal shock waves and turbulent boundary layers,ARC R&M 3262

Gartshore J S, Newman B G 1969Aeronaut. Q. 20: 25–56

Glusko G S 1965Bull. Acad. Sci. USSR Mech. Ser. (no. 4): 13–23

Grande E, Oates G C 1973 Unsteady flow generated by shock-turbulent boundary layer interactions,AIAA Paper 73-168

Green J E 1970Prog. Aerosp. Sci. 11: 235–340

Grin V T 1967Mech. Fluids Gases 6: 115–117 (in Russian)

Henderson L F 1967J. Fluid Mech. 30: 699–722

Horstmann C C, Hung C M 1979 Computation of three-dimensional turbulent separated flows at supersonic speeds,AIAA Paper 79-002

Horstmann C C, Owen F K 1974AIAA J. 12: 1436–1438

Hubbart J E, Bangert L H Turbulent boundary layer control by a wall jet,AIAA Paper 70-107

Hung C M, Kordulla W 1983 A time split finite volume algorithm for three-dimensional flow field simulations,AIAA Paper 83-1957

Inger G R 1981 Transonic shock/turbulent boundary layer interaction and incipient separation on curved surfaces.AIAA Paper 81-1244

Inger G R, Mason W H 1976AIAA J. 14: 1266–1272

Jones W P, Launder B E 1971Int. J. Heat Mass Transfer 15: 301–314

Kistler A L 1964J. Acoust. Soc. Am. 36: 543–550

Klineberg J M, Steger J L 1974 On laminar boundary layer separation,AIAA Paper 74-94

Kooi J W 1975 Flow separation,AGARD-CP-168, Paper no. 30

Kooi J W 1980Shock-boundary layer interaction in turbomachines, Von Karman Inst. (Belgium), Lecture Series 1980-8

Krishnamurthy V 1973Suppression of shock-induced separation using tangential fluid injection: Part I. M E Project Report, Dept. Aerosp. Eng., Indian Inst. Sci. Bangalore

Krogmann P, Stanewsky E, Thiede P 1984 Effect of local boundary layer suction on shock-boundary layer interaction and shock-induced separation,AIAA Paper 84-0098

Kuehn D M 1959 Experimental investigation of the pressure rise required for the incipient separation of turbulent boundary layers in two-dimensional supersonic flow,NASA Memo 1-21-59A

La Balleur J C 1981 Computation of viscous-inviscid interactions,AGARD CP 291, Paper No. 1

La Balleur J C 1984Numerical and physical aspects of aerodynamic flows II (Berlin: Springer Verlag)

La Balleur J C, Blaise D 1985Rech. Aerosp. (no. 4): 1–17

Lakshmikantha H, Yegna Narayan K, Srinivasan G 1969 Effect of fluid injection on shock-wave boundary layer interaction, Report 69FM 7, Dept. Aerosp. Eng., Indian Inst. Sci., Bangalore

Law C H 1974AIAA J. 12: 794–797

Lees L, Reeves B L 1964AIAA J. 2: 1907–1920

Levy L L 1978AIAA J. 14: 564–572

Lewis J E 1967Experimental investigation of supersonic laminar two-dimensional boundary layer separation in a compression corner with and without cooling, Ph D thesis, Cal. Inst. Technol.

Lewis J E, Kubota T, Lees L 1968AIAA J. 6: 7–14

Liepmann H W 1946J. Aeronaut. Sci. 13: 623–637

Liepmann H W 1947J. Aeronaut. Sci. 14: 295–302

Liepmann H W, Roshko A, Dhawan S 1951 On reflection of shock waves from boundary layers,NACA TN 2334

Lighthill M J 1953Proc R. Soc. London A217: 478–507

Lock R C 1981 Computation of viscous-inviscid interaction,AGARD CP 291, Paper no. 2

Manjunath A R 1973Supression of shock-induced separation using tangential fluid injection: Part II, M. E. Project Report, Dept. Aerosp. Eng., Indian Inst. Sci., Bangalore

Marvin J G 1982 Turbulence modelling for computational aerodynamics,AIAA Paper 82-0164

Marvin J G 1983 Modelling of turbulent separated flows for aerodynamic applications,NASA TM 84392

Mathews D C 1970Shock-wave boundary layer interactions in two-dimensional and axially-symmetric flows, Ph D thesis, University of Washington

McCormack R W 1976 An efficient numerical method for solving the time-dependent compressible Navier-Stokes equations at high Reynolds number,NASA TM X-73129

McCormack R W 1982AIAA J. 20: 1275–1281

McCormack R W, Lomax H 1979Annu. Rev. Fluid Mech. 11: 289–316

McDevitt J B 1979 Supercritical flow about a thick circular-arc airfoil.NASA TM 78549

McDevitt J B, Levy L L, Deiwert G S 1976AIAA J. 14: 606–613

McDonald H, Briley W R 1984Numerical and physical aspects of aerodynamic flows II (Berlin: Springer Verlag)

Mehta U, Lomax H 1982Prog. Astronaut. Aeronaut. 82: 297–375.

Meier G E A 1975 Flow separation,AGARD-CP-168. Paper no. 29

Melnik R E, Grossman B 1974 Analysis of interaction of a weak normal shock wave with a turbulent boundary layer,AIAA Paper 74-598

Melnik R E, Grossman B 1975Symp. Transonicum II (Berlin: Springer Verlag)

Melnik R E, Grossman B 1977Transonic problems in turbomachinery (New York: Hemisphere)

Messiter A F 1970SIAM J. Appl. Math. 18: 241–257

Narasimha R 1978 Turbulent flow separation: Two problems in application oriented research, Report 78FM 11, Dept. Aerosp. Eng., Indian Inst. Sci., Bangalore

Narasimha R, Prabhu A 1972J. Fluid Mech. 54: 1–17

Narasimha R, Sreenivasan K R 1973J. Fluid Mech. 61: 417–447

Neiland V 1969Fluid Dyn. (Engl. Transl.) 4: 33–35

Oskam B. Vas I E, Bogdonoff S M 1975 Flow separation,AGARD-CP-168, Paper no. 41

Pate S R 1969AIAA J. 7: 847–851

Peake D J 1966 The use of air injection to prevent separation of turbulent boundary layer in supersonic flow,ARC CP 890

Pearcey H H 1961Boundary layer and flow control (ed.) G V Lachmann (New York: Pergamon) vol. 2

Plotkin K J 1975AIAA J. 13: 1036–1040

Purohit S C 1987aJ. Spacecraft Rockets 23: 590–596

Purohit S C 1987bAIAA J. 25: 759–760

Rizetta D P, Burggraf O R, Jenson R 1978J. Fluid Mech. 89: 535–552

Rose W C 1973 The behaviour of a compressible turbulent boundary layer in a shock-wave induced adverse pressure gradient,NASA TN D-7092

Rose W C, Johnson D A 1975AIAA J. 13: 884–889

Roshko A, Thomke G J 1969Proc. Symp. on viscous interaction phenomena in supersonic and hypersonic flow (Univ. of Dayton Press) pp. 109–138

Roshko A, Thomke G J 1976AIAA J. 14: 873–879

Rotta J C 1968 Computation of turbulent boundary layers — 1968AFOSR-IFP, Stanford Conference, vol. I, pp 177–181

Rubesin M W 1982 The 1980–81AFOSR-HTTM-Stanford Conference on Complex Turbulent Flows: Comparison of Computation and Experiment. vol II, pp 713–719

Sagdeo P M 1974Suppression of shock-induced separation using tangential fluid injection, Part III: Effect of injection slot, M E Project Report. Dept. Aerosp. Eng., Indian Inst. Sci., Bangalore

Sandborn V A, Kline S J 1961J. Basic Eng. Trans. ASME 83: 317–327

Sawyer W G, East L F, Nash C R 1977 A preliminary study of normal shock wave turbulent boundary layer interaction.RAE Tech. Memo Aero. 1714

Schlichting H 1968Boundary-layer theory (New York: McGraw-Hill)

Schwendemann M F, Sanders B W 1982 Tangential blowing for control of strong normal shock-boundary layer interactions on inlet ramps.AIAA Paper 82-1082

Seddon J 1960 The flow produced by interaction of a turbulent boundary layer with a normal shock wave of strength sufficient to cause separation,ARC R&M 3502

Seddon J, Goldsmith E L 1985Intake aerodynamics (New York: Collins)

Seebaugh W R, Childs M E 1970J. Aircraft 7: 334–339

Seebaugh W R, Paynter G C, Childs M E 1968J. Aircraft 5: 461–467

Settles G S, Bogdonoff S M 1982AIAA J. 20: 782–789

Settles G S, Bogdonoff S M, Vas I E 1976aAIAA J. 14: 50–56

Settles G S, Perkins J J, Bogdonoff S M 1980AIAA J. 18: 779–785

Settles G S, Vas I E, Bogdonoff S M 1976bAIAA J. 14: 1709–1715

Shang J S, Hankey W L 1975AIAA J. 13: 1368–1374

Shang J S, Hankey W L, Law C H 1976AIAA J. 10: 1451–1457

Simpson R L, Strickland J H, Barr P W 1977J. Fluid Mech. 79: 553–594

Sirieix M 1975 Flow separation.AGARD-CP-168, Paper no. 12

Sirieix M, Delery J, Stanewsky E 1981Advances in fluid mechanics (New York: Springer Verlag)

Stanewsky E 1973Transonic flows in turbomachinery, Von Karman Institute (Belgium), Lecture Series 59

Stanewsky E, Nandanan M, Inger G R 1981 Computation of viscous-inviscid interactions,AGARD CP 291, Paper no. 4

Stewartson K 1974Adv. Appl. Mech. 14: 145–239

Stewartson K, Williams P G 1969Proc. R. Soc. London A312: 181–206

Sun C C, Childs M E 1974J. Aircraft 11: 54–59

Tanner L H, Gai S L 1970 Effects of suction on the interaction between shock wave and boundary layer at a compression corner,ARC CP 1087

Tassa Y, Sankar N L 1979AIAA J. 17: 1268–1270

Viegas J R, Horstmann C C 1978 Comparison of multi-equation turbulence models for several shock separated boundary layer interaction flows,AIAA Paper 78-1165

Veldman A E P 1984Computational methods in viscous flows (ed.) W G Habashi (Gedney,NY: Pineridge) vol. 3

Viswanath P R, Brown J L 1983AIAA J. 21: 801–807

Viswanath P R, Sankaran L, Sagdeo P M, Narasimha R 1977 Tangential blowing for control of shock-induced boundary layer separation: Review of recent IISc work, Report 77FM 11, Dept. Aerosp. Eng., Indian Inst. Sci., Bangalore

Viswanath P R, Sankaran L, Sagdeo P M, Narasimha R, Prabhu A 1983J. Aircraft 20: 726–732

Whitfield D L, Swafford T W, Jacocks J L 1981AIAA J. 19: 1315–1322

Wilcox D C, Rubesin M W 1980 Progress in turbulence modelling for complex flow fields including compressibility effects,NASA TP-1517

Wong W F 1974 The application of boundary layer suction to suppress strong shock-induced separation in supersonic inlets,AIAA Paper 74-1063

Wong W F 1977 Application of boundary layer blowing to suppress strong shock-induced separation in supersonic inlets,AIAA Paper 77-147

Wong W F, Hall G R 1975 Suppression of strong shock boundary layer interaction in supersonic inlets by boundary layer blowing.AIAA Paper 75-1209

Yegna Narayan K, Narasimha R 1973Aeronaut. Q. 24: 207–218