Interactions between shock waves and turbulent boundary layers

Progress in Aerospace Sciences

Volumn 11, Issue C, 1970, Pages

  Green, J E ^a  

^a Royal Aircraft Establishment   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 49849110318     PISSN: 03760421     EISSN: None     Source Type: Journal    
DOI: 10.1016/0376-0421(70)90018-7     Document Type: Article

References (78)

1. On the hypersonic laminar near wake critical point of the Crocco-Lees mixing theory
2. Integral theory for supersonic turbulent base flows
3. Separation of a supersonic turbulent boundary layer
4. Calculation of boundary layer development using the turbulent energy equation II: compressible flow on adiabatic walls
5. Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition
6. The prediction of separation and reattachment flow characteristics for two-dimensional supersonic and hypersonic boundary layers
7. The law of the wake in the turbulent boundary layer
8. Separated supersonic flow
9. A mixing theory for the interaction between dissipative flows and nearly isentropic streams
10. The peak pressure rise across an oblique shock emerging from a turbulent boundary layer over a plane surface
11. The calculation of three-dimensional turbulent boundary layers. Part 1: Flow over the rear of an infinite swept wing
12. Shock-boundary layer interaction and flow separation
13. Interactions between shock waves and boundary layers
14. Interactions between normal shock waves and turbulent boundary layers
15. An experimental investigation of the interaction between shock waves and boundary layers
16. Untersuchungen von Strahlspoilern im Uberschall im Hinblick auf eine Anwendung fur die Kraftstoffeinspritzung (Investigation on jet spoilers in the supersonic range with a view to an application for fuel injection)
17. Laminar boundary layer separation and near wake flow for a smooth blunt body at supersonic and hypersonic speeds
18. The turbulent boundary layer in two-dimensional flows with an oblique shock wave
19. Two-dimensional turbulent reattachment as a boundary layer problem
20. Reflection of an oblique shock wave by a turbulent boundary layer RAE TR 68256
21. Experimental studies on the lip shock
22. The interaction of shock waves and turbulent boundary layers
23. Scale effects in turbulent shock wave boundary layer interactions
24. Turbulent flow past two-dimensional bases in supersonic streams
25. Entrainment in the turbulent boundary layer
26. Lecture notes on the entrainment method
27. The reflexion of a shock wave at a rigid wall in the presence of a boundary layer
28. The distribution of a wall pressure rise in a turbulent boundary layer
29. An analytic study of separated flows induced by shock wave-boundary layer interaction
30. A theoretical investigation of the interaction between shock waves and boundary layers
31. A theoretical investigation of the interaction between shock waves and boundary layers
32. On the three-dimensional turbulent boundary layer generated by secondary flow
33. On the three-dimensional turbulent boundary layer generated by secondary flow
34. Supersonic turbulent boundary layer separation ahead of a wedge
35. Experimental investigation of the pressure rise required for the incipient separation of turbulent boundary layers in two-dimensional supersonic flow
36. Turbulent boundary layer separation induced by flares on cylinders at zero angle of attack
37. Supersonic separated and re-attaching flow 1 General theory and application to adiabatic boundary layer shock wave interactions
38. On boundary layers and upstream influence Part II-Supersonic flows without separation
39. Cross-flows produced by the interaction of a swept shockwave with a turbulent boundary layer
40. On the effect of Reynolds number on the peak pressure rise coefficient associated with separation of a turbulent boundary layer in supersonic flow
41. The three-dimensional interaction of a shock wave with a turbulent boundary layer
42. A study of the turbulent separated flow region occurring at a compression corner in supersonic flow
43. The interaction of a turbulent boundary layer and a shock at hypersonic Mach numbers
44. The isobars in boundary layers at supersonic speeds
45. An analysis of two-dimensional turbulent base flow, including the effect of the approaching boundary layer
46. A heat-transfer criterion for the detection of incipient separation in hypersonic flow
47. Theory of laminar separated flows on flared surfaces including supersonic flow with heating and cooling
48. Shock-induced separation and its prevention by design and boundary layer control
49. The interaction between local effects at the shock and rear separation—a source of significant scale effects in wind tunnel tests on aerofoils and wings
50. Effects of slot suction on turbulent boundary layer separation
51. Semi-empirical method for predicting effects of incident-reflecting shocks on the turbulent boundary layer
52. The determination of turbulent skin friction by means of pitot tubes
53. Theory of laminar near wake of blunt bodies in hypersonic flow
54. Effect of a discontinuity on turbulent boundary layer thickness parameters with application to shock induced separation
55. An introduction to the flow about plane sweptback wings at transonic speeds
56. Interaction of an oblique shock wave with a turbulent boundary layer
57. The flow produced by interaction of a turbulent boundary layer with a normal shock wave of strength sufficient to cause separation
58. Calculation of turbulent boundary layer characteristics across an oblique shock reflection including the effects of mass bleed
59. Recherches expérimentales fondamentales sur les écoulements séparés et applications
60. Basic experiments on the reattachment of a supersonic stream
61. The use of surface pitot tubes as skin-friction meters at supersonic speeds
62. The kinetic-energy-deficit equation of the turbulent boundary layer
63. An experimental investigation of the characteristics of some plane and cambered 65° delta wings at Mach numbers from 0·7 to 2·0
64. Sweepback effects in turbulent boundary layer shock wave interaction
65. An experimental study of the glancing interaction between a shock wave and a turbulent boundary layer
66. Correlated incompressible and compressible boundary layers
67. Further solutions of the Falkner-Skan equation
68. The determination of buffet boundaries of aerofoils
69. Rapid expansion of a supersonic boundary layer and its application to the near wake
70. On the singular points in the laminar two-dimensional near wake flow field
71. An exact treatment of the boundary layer equations describing the two-dimensional viscous analog of the one-dimensional inviscid throat