Hostname: page-component-586b7cd67f-rdxmf Total loading time: 0 Render date: 2024-12-03T19:14:23.712Z Has data issue: false hasContentIssue false
  • English
  • Français

50 years of turbomachinery research at Pyestock — part one: compressors

Published online by Cambridge University Press:  04 July 2016

J. Dunham
J. Dunham*
Affiliation:
Camberley, Surrey, UK
Get access Rights & Permissions [Opens in a new window]

Abstract

The two parts of this paper summarise the turbomachinery research undertaken at Pyestock during the 50 years since the National Gas Turbine Establishment was formed in 1946. The theoretical and experimental activities are described, and their influence on UK military and civil aero engines is assessed. The way in which NGTE supported non-aeronautical gas turbines is also explained. Part one provides a general introduction and then covers compressors.

Type
Research Article
Information
The Aeronautical Journal , Volume 104 , Issue 1033 , March 2000 , pp. 141 - 151
Copyright
Copyright © Royal Aeronautical Society 2000 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1. Andrews, S.J. Tests related to the effect of profile shape and camber line on compressor cascade performance, ARC R&M 2743, 1949.Google Scholar
2. Andrews, S.J., Jeffs, R.A. and Hartley, E.L. Tests concerning novel designs of blades for axial compressors, ARC R&M 2929, 1951.Google Scholar
3. Bryce, J.D., Cherrett, M.A. and Lyes, P.A. Three-dimensional flow in a highly loaded single-stage transonic fan, ASME Turbo, 1985, 117, p 22.Google Scholar
4. Calvert, W.J. An inviscid-viscous interaction treatment to predict the blade-to-blade performance of axial compressors with leading edge normal shock waves, ASME paper 82-GT-135, 1982.Google Scholar
5. Calvert, W.J. and Ginder, R.B. A quasi three-dimensional calculation system for the flow within transonic compressor blade rows, ASME paper 85-GT-22, 1985.Google Scholar
6. Calvert, W.J., Ginder, R.B., Mckenzie, I.R.I,and Way, D.J. Performance of a highly-loaded HP compressor, ASME paper 89-GT-24, 1989.Google Scholar
7. Came, P.M. The development, application and experimental evaluation of a design procedure for centrifugal compressors, Proc lMechE, 1978, 192, (5), p 49.Google Scholar
8. Carter, A.D.S. Three dimensional flow theories for axial compressors and turbines, Proc IMechE, 1948, 159.Google Scholar
9. Carter, A.D.S., Andrews, S.J. and Fielder, E.A. The design and testing of an axial compressor having a mean stage temperature rise of 30°C, ARC R&M 2985, 1953.Google Scholar
10. Carter, A.D.S. A theoretical investigation of the factors affecting stalling flutter of compressor blades, ARC CP 265, 1955.Google Scholar
11. Carter, A.D.S. and Ktlpatrick, D.A. The self-excited vibration of axial- flow compressor blades, Proc IMechE, 1956, 171, (7).Google Scholar
12. Carter, A.D.S., Turner, R.C., Sparkes, D.W. and Burrows, R.A. The design and testing of an axial flow compressor having different blade profiles in each stage, ARC R&M 3183, 1957.Google Scholar
13. Cherrett, M.A. and Bryce, J.D. Unsteady viscous flow in a high speed core compressor, ASME Turbo, 1992, 114, p 287.Google Scholar
14. Constant, H. Early history of the axial type of gas turbine engine, Proc IMechE, 1945, 153.Google Scholar
15. Dransfield, D.C. and Calvert, W.J. Detailed flow measurements in a four stage axial compressor, ASME paper 76-GT-46, 1976.Google Scholar
16. Dunham, J., Flitcroft, J.E. and Abbott, W.A. Transmission of inlet distortion through a fan, AGARD CP 400, paper 13, 1986.Google Scholar
17. Dunham, J. A new endwall model for axial compressor throughflow calculations, ASME Turbo, 1995, 117, p 533.Google Scholar
18. Dunham, J. A.R.Howell — father of the British axial compressor, ASME paper 2000-GT-0008, 2000.Google Scholar
19. Frost, D.H. A streamline curvature through-flow computer program for analysing the flow through axial-flow turbomachines, ARC R&M 3687, 1970.Google Scholar
20. Ginder, R.B. and Newby, D.R. A study of factors affecting the broadband noise of high speed fans, Aircraft, 1977, 14, (9).Google Scholar
21. Ginder, R.B., Kenison, R.C. and Smith, A.D. Considerations for the design of inlet flow conditioners for static fan noise testing, AIAA paper 79-0657, 1979.Google Scholar
22. Ginder, R.B. Design and performance of advanced blading for a high speed HP compressor, ASME paper 91-GT-374, 1991.Google Scholar
23. Herbert, M.V. A method of performance prediction for centrifugal compressors, ARC R&M 3843, 1978.Google Scholar
24. Howell, A.R. (a) Design of axial compressors, (b) fluid dynamics of axial compressors, Proc IMechE, 1945, 153.Google Scholar
25. Howell, A.R. and Bonham, R.P. Overall and stage characteristics of axial flow compressors, Proc IMechE, 1950, 163.Google Scholar
26. Howell, A.R. and Calvert, W.J. A new stage stacking technique for axial-flow compressor performance prediction, ASME Eng Power, 1978, 100, p 698.Google Scholar
27. Marsh, R. A digital computer program for the through-flow fluid mechanics in an arbitrary turbmachine using a matrix method, ARC R&M 3509,1966.Google Scholar
28. Philpot, M.G. The buzz-saw noise generated by a high duty transonic compressor, ASME Eng Power, 1971, 93, Ser A, (1), p 63.Google Scholar
29. Ringrose, J. Half-speed bearing whirl excited by a single propagating stall cell in a multistage axial-flow compressor, ARC R&M 3598, 1967.Google Scholar
30. Smith, D.J.L. and Frost, D.H. Calculation of the flow past turbomachine blades, Proc IMechE, 1970, 184, pt 3G, paper 27.Google Scholar
31. Turner, R.C. and Jefferson, J.L. Some shrouding and tip clearance effects in axial flow compressors, NE Coast Inst Engrs Shiprs, 1958, 74.Google Scholar