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Effect of heat transfer on periodic transonic flows

Published online by Cambridge University Press:  04 July 2016

D. A. Mitchell ,
R. K. Cooper  and
S. Raghunathan
D. A. Mitchell
Affiliation:
School of Aeronautical Engineering, The Queen's University of Belfast, UK
R. K. Cooper
Affiliation:
School of Aeronautical Engineering, The Queen's University of Belfast, UK
S. Raghunathan
Affiliation:
School of Aeronautical Engineering, The Queen's University of Belfast, UK
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Abstract

The effects of the model surface to free stream adiabatic temperature ratio (Tw/Tad) on periodic transonic flow over a 14% thick biconvex aerofoil are evaluated using a computational fluid dynamic approach. The analysis is based on the thin layer Navier Stokes equations with Baldwin-Lomax turbulence model. The results of computations showed that on biconves aerofoils there is a large effect of heat transfer on instantaneous pressure distributions and periodic buffet excitation level confirming some of the available experimental data. The effects observed have an implication in wind tunnel measurement of buffet associated periodic transonic flows.

Type
Research Article
Information
The Aeronautical Journal , Volume 103 , Issue 1025 , July 1999 , pp. 329 - 337
Copyright
Copyright © Royal Aeronautical Society 1999 

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References

1. van driest, E.R. Convective heat transfer in gases, In: Turbulent Flows and Heat Transfer in High Speed Aerodynamics and Jet Propulsion, Section, F. Vol 5, Oxford University Press, 1969.Google Scholar
2. Dougherty, N.S. and Fisher, D.F. Boundary layer transition on a 10° cone: wind tunnel and flight test correlation, AIAA Paper 80-01544, 1980.Google Scholar
3. Liepmann, H.W. and Fila, G.H. Investigations of effect of surface temperature and single roughness elements on boundary layer transition, NACA TN 1196, 1947.Google Scholar
4. Macha, J.M., Norton, D.J. and Young, J.C. Surface temperature effects on subsonic stall, AIAA Paper 72–960, 1972.Google Scholar
5. Lynch, F.T., Faucher, M.F., Patel, D.R. and Inger, G.R., Adiabatic model wall effects on transonic airfoil performance in cryogenic wind tunnels, AGARD CP 348, Paper 14, 1983.Google Scholar
6. Frishett, J.C. Incipient Separation of a Supersonic Turbulent Boundary layer Including Effects of Heat Transfer, PhD Thesis, University of California, 1971.Google Scholar
7. Elfstrom, G.M. Turbulent separation in hypersonic flow, Imperial College of Science and Technology, Aero Report 71–16,1971.Google Scholar
8. Inger, G.R., Lynch, F.T. and Faucher, M.F. A theoretical and experimental study on non-adiabatic wall effects on transonic shock-boundary-layer interaction, AIAA Paper 83–1421, 1983.Google Scholar
9. Delery, J.M. Shock wave-turbulent boundary layer interaction and its control, Prog Aerospace Sci, 1985,22, pp 209–280.Google Scholar
10. Raghunathan, S., and Mitchell, D. Computed effects of heat transfer on transonic flows. AIAA J, 1995,33, (11), pp 2120–2127.Google Scholar
11. Green, J.E., Weeks, D.J. and Pugh, P.G. Heat transfer as a source of spurious scale effects in subsonic and transonic wind tunnels, ARC 38182, May 1979.Google Scholar
12. Mabey, D.G. Effects of heat transfer in aerodynamics and possible implications for wind tunnel tests, Progress in Aerospace Sciences, 1991,27, (4), pp 267–303.Google Scholar
13. Mcdevitt, J.B. Supercritical flow about a thick circular aerofoil, NASA TM 78549, 1979.Google Scholar
14. Mabey, D.G. Oscillatory flow from shock induced separation on biconvex aerofoils of varying thickness in ventilated wind tunnels, AGARD CP 296, Paper 11, 1980.Google Scholar
15. Mabey, D.G, Welsh, B.L., and Cripps, B.E. Periodic flow on a rigid 14% thick biconvex wing at transonic speeds, RAE TR 81–059, 1981.Google Scholar
16. Edwards, J. Transonic shock oscillations calculated with a new interactive boundary layer coupling method, AIAA, Paper 93–0777, 1993.Google Scholar
17. Raghunathan, S., Zarifi-rad, F. and Mabey, D.G. Investigations on the effect of model cooling on transonic flows, AGARD, Conference Proceedings, 507, Paper 26, 1992.Google Scholar
18. Raghunathan, S., Hall, D.E. and Mabey, D.G. Alleviation of shock oscillations in transonic flow by passive control, Aeronaut J, August/September 1990,94, (937), pp 245–250.Google Scholar
19. Tudeman, H. Investigations of the periodic flow around oscillating aerofoils, National Aerospace Lab, The Netherlands, NLR TR 77090 U, 1977.Google Scholar
20. Baldwin, B.S. and Lomax, H. Thin layer approximation and algebraic model for separated turbulent flows, AIAA, Paper 78–0257, 1978.Google Scholar
21. Maccormack, R.W. Current status of numerical solutions of the Navier-Stokes equations, AIAA Paper 85–0032, 1985.Google Scholar
22. van leer, B. Flux vector splitting for the Euler equations, ICASE Report 82–30, 1982.Google Scholar
23. Mulder, W.A. and van leer, G. An implicit finite-difference algorithm for hyperbolic systems in conservation-law-form, J Comp Phys, 1976,32, pp 87–110.Google Scholar
24. Cook, P.H., MacDonald, M.A. and Firmin, M.C.P. Aerofoil RAE2822- pressure distribution and boundary layer and wake measurements, AGARD-AR-138,1979.Google Scholar
25. Mitchell, R.D. A Computational Study of Heat Transfer on Transonic Flow Over an Aerofoil, PhD Thesis, School of Aeronautical Engineering, The Queen's University of Belfast, 1993.Google Scholar
26. Maksymiuk, C.M. and Pulliam, T.H. Viscous transonic airfoil work shop results using ARC2D, AIAA Paper 87-0415, 1987.Google Scholar
27. Harris, C.D. Two-dimensional aerodynamic characteristics of the NACA0012 airfoil in the Langley 8-foot transonic pressure tunnel, NASA-TM-81927, 1981.Google Scholar
28. Spalding, D.B. and Chi, S.W. The drag of a compressible turbulent boundary layer on a smooth flat plate with and without heat transfer, J Fluid Mech, 1964,18, pp 117–143.Google Scholar
29. Pappas, C.C. Measurement of heat transfer in the turbulent boundary layer on a flat plate in supersonic flow and comparison with skin friction results, NACA TN 3222, 1954.Google Scholar
30. Mcdevitt, J.B., Levy, L.L. and Deiwerf, G.S. Transonic flow about a thick circular arc airfoil, AIAA J, 1976,14, pp 606–613.Google Scholar
31. Levy, L.L. Experimental and computational steady and unsteady transonic flows about a thick airfoil, AIAA J, 1978,16, pp 564–572.Google Scholar
32. Edwards, J.W. Transonic shock oscillations calculated with a new interactive boundary layer coupling method, AIAA Paper 93–0777, 1993.Google Scholar
33. Steger, J.L. Implicit finite difference simulation of flow about arbitrary two dimensional geometry, AIAA J, 1978, 16, (7), pp 679–686.Google Scholar
34. Mohan, S.R. Periodic flow over rigid aerofoils at transonic speeds, AIAA paper, 91–0598,1991.Google Scholar
35. Nixon, D., Caruso, S.C. and Farshchi, M. Further study of phantom solutions to the TSD-Euler equation, Acta Mechanica, 1991,86, pp 15–29.Google Scholar