A review of the role of some small high-speed wind tunnels in aeronautical research

Progress in Aerospace Sciences

Volumn 34, Issue 3-4, 1998, Pages 107-166

  Squire, L C ^a  

^a CHURCHILL COLLEGE   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; REYNOLDS NUMBER; SUPERSONIC AERODYNAMICS; SUPERSONIC AIRCRAFT; SUPERSONIC FLOW;

HIGH SPEED BLOWDOWN TUNNELS;

WIND TUNNELS;

EID: 0032010677     PISSN: 03760421     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0376-0421(98)00001-3     Document Type: Article

References (110)

1. Andersen, P.S., Kays, W. M. and Moffat, R. J. (1972) The turbulent boundary layer on a porous plate: An experimental study of the fluid mechanics for adverse free stream pressure gradients. Report No. HMT-15, Thermosciences Division, Dept. of Mech. Eng., Stanford University.
2. Atkin, C. J. (1990) A numerical study of unsteady shock/boundary layer interactions Ph.D. Dissertation, University of Cambridge.
3. Atkin, C. J. and Squire, L. C. (1992) A study of the interaction of a normal shock wave with a turbulent boundary layer at Mach numbers between 1.30 and 1.55. European J. Mech. B. Fluids 11, 93-118.
4. Baker, C. J. and Squire, L. C. (1981) Turbulent boundary layer development on a two-dimensional aerofoil with supercritical flow at low Reynolds numbers. Aeronautical Quart. 33, 174-198.
5. Bartle, E. R. and Leadon, B. M. (1991) Experimental evaluation of heat transfer with transpiration cooling in a turbulent boundary layer at M = 3.2. J. Aerospace Sci. 27, 78-80.
6. Bowman, I.N. R. (1991) A study of mass injection into an axisymmetric supersonic wake. Ph.D. Dissertation, University of Cambridge.
7. Bryanston Cross, P. J. (1986) High speed flow visualization. Prog. Aerospace Sci. 23, 85-104.
8. Butler, D.S. (1960) The numerical solution of hyperbolic systems of partial differential equations in three independent variables. Proc. Roy. Soc. 255, 232-252.
9. Chew, Y. T. (1976) The turbulent boundary layer at an expansion corner with shock waves. Ph.D. Dissertation, University of Cambridge.
10. Chew, Y. T. (1979) Shockwave and boundary layer interaction in the presence of an expansion corner. Aeronautical Quart. 30, 506-527.
11. Chew, Y. T. and Squire, L. C. (1978) The boundary-layer development downstream of a shock at an expansion corner. ARC R & M 3839.
12. Chokani, N. (1988) A study of the passive effect on transonic shockwave-turbulent boundary layer interactions on porous surfaces. Ph.D. Dissertation, University of Cambridge.
13. Chokani, N. and Squire, L.C. (1993) Transonic shockwave/turbulent boundary layer interactions on a porous surface. Aeronautical J. 97, 163-170.
14. Coles, D. E. (1954) Measurements of turbulent friction on a smooth flat plate in supersonic flow. J. Aerospace Sci. 21, 433-448.
15. Crocco, L. (1932) Su di un valor massimo del coefficiente di trasmissione del calore da una lamina piana a un fluido scorrente L'Aerotecnica, 12, 181-197.
16. Danberg, J. E. (1964) Characteristics of the turbulent boundary layer with heat and mass transfer at M = 6.7. NOLTR 64-99.
17. Dawes, W. N. (1979) A study of shock waves in three-dimensional transonic flow. Ph.D. Dissertation, University of Cambridge.
18. Dawes, W. N. and Squire, L. C. (1982) A study of shock waves in three-dimensional flow. J. Fluids Engng 104, 393-399.
19. Delery, J. M. (1985) Shock wave/turbulent boundary layer interaction and its control. Prog. Aerospace Sci. 22, 209-280.
20. Dershin, H., Leonard, C. A. and Gallaher, W. H. (1967) Direct measurement of skin-friction on a porous flat plate with mass transfer. AIAA J. 5, 1934-36.
21. Dunbar, D. I. A. (1968) Turbulent boundary layers with foreign gas injection. Ph.D. Dissertation, University of Cambridge.
22. Dunbar, D. I. A. and Squire, L. C. (1972) Experiments in turbulent boundary layers with foreign gas injection. ARC R and M 3696.
23. East, L. F., Sawyer, W. G. and Nash, C. R. (1979) An investigation of the structure of equilibrium turbulent boundary layers. R.A.E. Tech. Report 79040.
24. Edwards, J. A., Bryanston-Cross, P. J. and Squire, L. C. (1986) Experimental observations on unsteady, normal shock/boundary layer interactions. Proc. AGARD Conf. on Transonic and Supersonic Phenomena in Turbomachines, PEP 68B, 1986.
25. Edwards, J. A. and Squire, L. C. (1993) An experimental study of the interaction of an unsteady shock with a turbulent boundary layer at Mach numbers of 1.3 and 1.5. Aeronautical J. 97, 337-348.
26. Fanourakis, P. (1993) Rough surfaces with drag reducing properties in turbulent flow. M.Sc Dissertation, University of Cambridge.
27. Faucher, X. (1995) Passive control of swept shock/boundary layer interactions. Unpublished Cambridge University Engineering Department Thesis.
28. Finley, P. J. (1963) Experiments on jets directed from blunt bodies. Ph.D. Dissertation, University of Cambridge.
29. Finley, P. J. (1966) The flow of a jet from a body opposing a supersonic stream. J. Fluid Mech. 26, 337-368.
30. Fernholz, H. H and Finley, P. J. (1977) A critical compilation of compressible boundary layer data. AGARD Report Ag-223.
31. Fernholz, H. H. and Finley, P. J. (1980) A critical commentary on mean flow data for two-dimensional compressible turbulent boundary layer. AGARD Report Ag-253.
32. Fernholz, H. H and Finley, P. J. (1981) A further compilation of compressible boundary layer data with a survey of turbulence data. AGARD Report Ag-263.
33. Gibson, T. (1997) Two-dimensional shock/boundary-layer interactions with passive control. Ph.D. Dissertation, University of Cambridge.
34. Green, J.E. (1963) The turbulent boundary layer in a two-dimensional flow with an oblique shock wave. Ph.D. Dissertation, University of Cambridge.
35. Green, J. E. (1968) Reflection of an oblique wave by a turbulent boundary layer. J. Fluid Mech. 40, 81-95.
36. Green, J. E. (1970) Interactions between shock waves and turbulent boundary layers. Prog. Aerospace Sci. 11, 234-340.
37. Hayawaka, K. (1979) The effect of upstream boundary layer state on the shock interaction at a compression corner. Ph.D. Dissertation, University of Cambridge.
38. Hayawaka, K. and Squire, L. C. The effect of upstream boundary layer state on the shock interaction at a compression corner. J. Fluid Mech. 122, 368-394.
39. Hinchliffe, R. A. (1993) The interaction of a normal shock with a non-equilibrium boundary layer. Ph.D. Dissertation, University of Cambridge.
40. Hillier, R. (1970) Some applications of thin shock layer theory to hypersonic wings. Ph.D. Dissertation, University of Cambridge.
41. Hillier, R. (1970) The effects of yaw on conical wings at high supersonic speeds. Aeronautical Quart. XXI, 199-210.
42. Hillier, R. (1972) Pressure distributions at M = 3.51 and at high incidence for four wings of delta planform. ARC Current Paper 1198.
43. Hillier, R. (1972) Three-dimensional wings in hypersonic flow. J. Fluid Mech. 54, 305-337.
44. Holmes. S. C. (1990) An investigation of supersonic flow over a compression corner Ph.D. Dissertation, University of Cambridge.
45. Hustad, C.-W. and Squire, L. C. (1995) Application of holographic interferometry for evaluation 3D Navier-Stokes calculations. Expt. Fluids 18, 343-359.
46. Jackson, M. W., Czarnecki, K. R. and Monta, W. J. (1965) Turbulent skin friction at high Reynolds number and low supersonic velocities. NASA Tech Note D-2896.
47. Jeromin, L. O. F. (1966) Compressible turbulent boundary layers with air injection. Ph.D. Dissertation, University of Cambridge.
48. Jeromin, L. O. F. (1966) An investigation of compressible turbulent boundary layers with air injection. ARC R & M 3526.
49. Kays, W. and Moffat, R. J. (1975) The behaviour of transpired turbulent boundary layers Report No. HMT-22, Thermosciences Division, Dept. of Mech. Eng., Stanford University.
50. Kubota, H. and Stollery, J. L. (1982) An experimental investigation of the interaction between a glancing shock wave and a turbulent boundary layer. J. Fluid Mech. 116, 431-458.
51. Kuehn, D. M. (1959) Experimental investigation of the pressure rise required for incipient separation of turbulent boundary layers in two-dimensional supersonic flow. NASA Memo 1-21-59A.
52. Leadon, B. M. and Scott, C. J. (1956) Transpiration cooling experiments in a turbulent boundary layer at M = 3. J. Aerospace Sci. 23, 798-799.
53. Leung, A. W. C. (1993) An investigation of three-dimensional shockwave/ turbulent boundary layer interaction. Ph.D. Dissertation, University of Cambridge.
54. Leung, A. W. C. and Squire, L. C. (1995) Reynolds number effects in swept-shock-wave/turbulent-boundary-layer interaction. AIAA J. 33, 798-804.
55. Liu, X. (1985) Shock/boundary-layer interactions on curved surfaces at transonic speeds. Ph.D. Dissertation, University of Cambridge.
56. Liu, X. and Squire, L. C. (1988) An investigation of shock/boundary-layer interactions on curved surfaces at transonic speeds. J. Fluid Mech. 187, 467-486.
57. Lowrie, B. W. (1965) Cross-flows produced by the interaction of a swept shockwave with a turbulent boundary layer. Ph.D. Dissertation, University of Cambridge.
58. Mabey, D. G. and Sawyer, W.G. (1976) Experimental studies of the boundary layer on a flat plate at Mach numbers from 2.5 to 4.6. R & M No 3784.
59. Marriott, P. G. (1973) Compressible turbulent boundary layers with discontinuous injection. Ph.D. Dissertation, University of Cambridge.
60. Marriott, P. G. (1974) Compressible turbulent boundary layers with discontinuous air injection. ARC R & M 3780.
61. Moore, D. R. and Harkness, J. (1964) Experimental investigation of the compressible turbulent boundary layer at very high Reynolds number, M = 2.8. AIAA paper 64-592.
62. Narayan, K. Y. (1974) Wings with curved leading edges at supersonic speeds. Ph.D. Dissertation, University of Cambridge.
63. Narayan, K. Y. Effects of yaw on a gothic wing at supersonic speeds. Aeronautical Quart. XXV, 119-128.
64. Narayan, K. Y. (1975) The flow over a "high" aspect ratio gothic wing at supersonic speeds. Aeronautical Quart. XXVI, 189-202.
65. Narayan, K. Y. (1974) Pressure distributions on two wings with curved leading edges at supersonic speeds. ARC R & M 3741.
66. Narayan, K. Y. and Seshadri, S. N. (1997) Types of flow on the lee side of delta wings. Prog. Aerospace Sci. 33, 167-258.
67. Pearcey, H. H., Osborne, J. and Haines, A. B. (1968) The interaction between local effects at the shock and rear separation - a source of significant scale effect in wind tunnel tests on aerofoils and wings. AGARD CP 35, Paper 11.
68. Popinski, Z and Ehrlich, C. F. (1966) Development design method for predicting hypersonic aerodynamic control characteristics. USAF Tech. Report. AFFDL-TR-66-85.
69. Ragunathan, S. (1988) Passive control of shock-boundary layer interaction. Prog. Aerospace Sci. 25, 271-296
70. Sabjen, M. and Crites, R. C. (1979) Real time optical measurements of time dependent shock position. AIAA J. 17, 910-912.
71. Sandeman, R. (1979) Studies of wall interference in transonic tunnels. Ph.D. Dissertation, University of Cambridge.
72. Sawyer, W. G. and Long, C. J. (1982) A study of normal shockave turbulent boundary-layer interaction at Mach numbers of 1.3, 1.4 and 1.5. RAE TR 82099.
73. Settles, G. S. and Dolling, D. S. (1986) Swept shock wave/boundary-layer interactions. In AIAA Progress in Aeronautics and Astronautics: Tactical Missile Aerodynamics, Vol. 104, pp. 297-379 (eds M. Hemsch and J. Neilsen). AIAA, New York.
74. Shutts, W. H., Hartwig, W. H. and Weiler, J. E. (1955) Turbulent boundary layer and skin-friction measurements on a smooth thermal insulated flat plate at supersonic speeds. Texas Univ. Report DRL-364.
75. Smith, M. G. (1977) Interaction of a shockwave with a boundary layer disturbed by injection. Ph.D. Dissertation, University of Cambridge.
76. Spalding, D. A., Auslander, D. M. and Sundaram, T. R. (1964) The calculation of heat and mass transfer through the turbulent boundary layer on a flat plate at high Mach numbers, with and without chemical reaction. In: Supersonic Flow, Chemical Processes and Radiative Transfer (Eds D. B. Olfe and V. Zzkkay) Pergamon Press, Oxford.
77. Spence, D. A. (1960) Velocity and enthalpy distributions in the compressible turbulent boundary layer on a flat plate. J. Fluid Mech. 8, 368-387.
78. Squire, L. C. (1968) A law of the wall for compressible turbulent boundary layers with air injection. J. Fluid Mech. 37, 449-456.
79. Squire, L. C. (1968) Calculation of the pressure distributions on lifting conical wings with applications to the off-design behaviour of waveriders. AGARD CP 30. Paper 11
80. Squire, L. C. (1970) Further experimental investigations of compressible turbulent boundary layers with air injection. ARC R & M 3637.
81. Squire, L. C. (1974) Some extensions of thin-shock-layer theory. Aeronautical Quart. XXV, 1-13.
82. Squire, L. C. (1975) The effects of recessed lower surface shape on the lift and drag of conical wings at high incidence and high Mach number. Aeronautical Quart. XXVI, 1-9.
83. Squire, L. C. (1981) Measured pressure distributions and shock shapes on a simple delta wing. Aeronautical Quart. XXXII, 188-198,
84. Squire, L. C. (1985) Leading edge separations and cross-flow shocks on delta wings at supersonic speeds. AIAA J. 23, 321-325.
85. Squire, L. C. (1986) Effect of probe supports on measurements in steam turbines. ASME Paper 86-Gt-213.
86. Squire, L. C. (1995) Measurement of drag using a momentum balance. Aeronautical J. 99, 183-186.
87. Squire, L. C., Bryanston-Cross, P.J. and Liu, X. (1991) An interferometric study of the shock interaction at a compression corner. Aeronautical J. 95, 143-151.
88. Squire, L.C. and Nasser, S. (1993) Cavity drag at transonic speeds. Aeronautical J. 97, 247-256.
89. Squire, L. C. and Savill, A. M. (1989) Drag measurements on planar riblet surfaces at high subsonic speeds. Appl. Sci. Res. 46, 229-243.
90. Squire, L. C. and Savill, A. M. (1996) Experimental results on aerofoil manipulators at high subsonic speeds. Expt. Fluids. 21, 275-285,
91. Squire, L. C. and Smith, M. G. (1980) Interaction of a shock wave with a turbulent boundary layer disturbed by injection. Aeronautical Quart. 31, 86-112.
92. Stevenson, T. N. (1964) A law of the wall for boundary layers with suction or injection. College of Aeronautics, Cranfield, Report Aero. No. 166.
93. Szodruch, J. (1977) Leeseiten-strömung bei schlanken deltaflügeln dicke. ILR Bericht 23, Techn. University of Berlin.
94. Thomas, G. D. (1972) Compressible turbulent boundary layers with combined air injection and pressure gradient. Ph.D. Dissertation, University of Cambridge.
95. Thomas, G. D. (1974) Compressible turbulent boundary layers with combined air injection and pressure gradient. ARC R & M 3779.
96. van Driest, E. R. (1951) Turbulent boundary layers in compressible flow. J. Aerospace Sci. 18, 145.
97. Voisient, R. L. P. (1979) Combined influence of roughness and mass transfer on turbulent skin friction at M = 2.9. AIAA Paper 79-0003.
98. Watterson, J. (1996) A new pressure-based Navier-Stokes solver, and application to 3D compressible vortex/boundary layer interactions. Ph.D. Dissertation, University of Cambridge.
99. Winter, K. G. and Gaudet, L. (1970) Turbulent boundary-layer studies at high Reynolds numbers at Mach numbers between 0.2 and 2.8 ARC R & M 3712.
100. Xu, L. (1985) The base pressure and trailing edge loss of transonic turbine blades. Ph.D. Dissertation, University of Cambridge.
101. Yeung, A. F. K. (1994) The passive control of swept-shock/boundary layer interactions. Ph.D. Dissertation, University of Cambridge.
102. Young, A. D. and Paterson, J. H. (1981) Aircraft excrescence drag. AGARDograph No. 264.
103. Zhang, X. (1987) An experimental and computational investigation into supersonic shear layer driven single and multiple cavity flowfields. Ph.D. Dissertation, University of Cambridge.
104. Zhang, X. and Edwards, J. A. (1988) Computational analysis of unsteady supersonic cavity flows driven by thick shear layers. Aeronautical J. 92, 365-374.
105. Zhang, X. and Edwards, J.A. (1990) An investigation of supersonic oscillatory cavity flows driven by thick shear layers. Aeronautical J. 94, 355-364.
106. Zhang, X. and Edwards, J.A. (1992) Experimental investigation of supersonic flow over two cavities in tandem. AIAA J. 30, 1182-1190.
107. Zhang, X. (1995) Compressible cavity flow oscillations due to shear layer instabilities and pressure feedback. AIAA J. 33, 1404-1411.
108. Zhong, S. (1993) An interferometric study of organised structures in compressible turbulent flow. Ph.D. Dissertation, University of Cambridge.
109. Zhong, S. and Squire, L. C. (1995) An interferometric study of organised structures in wakes of circular cylinders. Expt. Fluids 20, 91-99.
110. Zhong, S. and Squire, L. C. (1995) Interferometric study of organised motions in turbulent boundary layers. AIAA J. 33, 439-444.