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The High Temperature Turbo-jet Engine

Published online by Cambridge University Press:  28 July 2016

D. G. Ainley
D. G. Ainley*
Affiliation:
National Gas Turbine Establishment
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Extract

The 985th Lecture to be given before the Society, “ The High Temperature Turbo-jet Engine ” by D. G. Ainley, B.Sc, A.M.I.Mech.E., A.F.R.Ae.S., was given at the Institution of Civil Engineers, Great George St., London, S.W.I on 15th March 1956, with Mr. N. E. Rowe, C.B.E., D.I.C., F.C.G.I., F.I.A.S., F.R.Ae.S., in the Chair. Introducing the Lecturer, Mr. Rowe said that Mr. Ainley had been working on gas turbines since 1943 when he joined the gas turbine division of the Royal Aircraft Establishment. He transferred to Power Jets Ltd. and later to the National Gas Turbine Establishment. His early work was associated with the development of axial flow compressors, contraction design and so on; he then transferred to turbine design, became head of the section dealing with turbine and heat transfer problems and for the past five or six years had been chiefly engaged on the cooling of gas turbine blades. Mr. Ainley graduated from the University of London, Queen Mary College, with first class honours. In 1953 he was awarded the George Stephenson Research Prize by the Institution of Mechanical Engineers.

Type
Research Article
Information
The Aeronautical Journal , Volume 60 , Issue 549 , September 1956 , pp. 563 - 589
Copyright
Copyright © Royal Aeronautical Society 1956

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References

1. Fozard, J. W. (1954). The Supersonic Fighter. Flight Vol. 66, No. 2394-2396 (1954).Google Scholar
2. McAdams, W. H. (1942). Heat Transmission. McGraw-Hill (1942).Google Scholar
3. Eckert, E. R. G. (1950). Introduction to the Transfer of Heat and Mass. McGraw-Hill (1950).Google Scholar
4. Squire, H. B. (1942). Heat Transfer Calculations for Aerofoils. A.R.C. R.& M. No. 1986 (1942).Google Scholar
5. Wilson, D. G. and Pope, J. A. (1954). Convective Heat Transfer to Turbine Blades Surfaces. Proc. I. Mech E. Vol. 168, No. 36 (1954).Google Scholar
6. Ainley, D. G. (1955). Internal Air-cooling for Turbine Blades. A General Design Survey. Unpublished N.G.T.E. Note (1955).Google Scholar
7. Andrews, S. J. and Bradley, P. C. (1948). Heat Transfer to Turbine Blades. N.G.T.E. Memo No. M37 (1948).Google Scholar
8. Hubbart, J. E. (1950). Comparison of Outside Surface Heat Transfer Coefficients for Cascades of Turbine Blades. N.A.C.A. R.M. E50C28 (1950).Google Scholar
9. Bammert, K. and Hahnemann, H. A. (1946). Heat Transfer in Gas Surrounding Cooled Gas Turbine Blades. Pt. III. R.T.P. No. 620; G.D.C. 2466 (M.O.S.) (1946).Google Scholar
10. Pohleman, E. (1947). Temperatures and Stresses on Hollow Blades for Gas Turbines. N.A.C.A. T.M. 1183 (1947).Google Scholar
11. Smith, A. G. (1948). Heat Flow in the Gas Turbine. Proc. I. Mech. E., Vol. 159 (1948).CrossRefGoogle Scholar
12. Reeman, J., Buswell, R. W. and Ainley, D. G. (1953). An Experimental Single-stage Air-cooled Turbine. Proc. I. Mech. E., Vol. 167 (1953).Google Scholar
13. Adderley, J. W. (1949). German Gas Turbine Developments during the Period 1939 to 1945. B.I.O.S. Overall Report No. 12, H.M.S.O. (1949).Google Scholar
14. Sproule, R. S. (1946). Outline of Present Knowledge; Concerning Hollow Blades for Gas Turbines. Issued by R.T.P./T.I.B. A.R.C. No. 9682 (1946).Google Scholar
15. Kohlmann, H. (1950). The Development of a Hollow Blade for Exhaust Gas Turbines. N.A.C.A. T.M. No. 1289 (1950).Google Scholar
16. Schey, O. W. (1948). The Advantages of High Inlet Temperatures for Gas Turbines and Effectiveness of Various Methods of Cooling the Blades. A.S.M.E. Paper No. 48-A-105 (1948).Google Scholar
17. Silverstein, A. (1949). Research on Aircraft Propulsion Systems. Journal of the Aeronautical Sciences, Vol. 16, No. 4 (1949).Google Scholar
18. Ellerbrock, H. (1951). N.A.C.A. Investigations of Heat Transfer of Cooled Gas Turbine Blades. General Discussion on Heat Transfer. Proc. I. Mech. E. (1951).Google Scholar
19. Ellerbrock, H. and Stepka, F. S. (1950). Experimental Investigation of Air-cooled Turbine Blades in Turbo-jet Engine. I.—Rotor Blades with 10 Tubes in Cooling Air Passages. N.A.C.A. R.M. E50I04 (1950).Google Scholar
20. Hickel, R. O. and Ellerbrock, H. (1950). Experimental Investigation of Air-cooling Turbine Blades in Turbo-jet Engine. II.—Rotor Blades with 15 Fins in Cooling Air Passages. N.A.C.A. R.M. E50I14 (1950).Google Scholar
21. Arne, V. L. and Esgar, J. B. (1951). Experimental Investigation of Air-cooled Turbine Blades in Turbo-jet Engine. VI.—Conduction and Film Cooling of Leading and Trailing Edges of Rotor Blades. N.A.C.A. R.M. E51C29 (1951).Google Scholar
22. Long, R. A. and Esgar, J. B. (1951). Experimental Investigation of Air-cooled Turbine Blades in Turbo-jet Engine. VII.—Rotor Blade Fabrication Procedures. N.A.C.A. R.M. E51E23 (1951).Google Scholar
23. Stepka, F. S. and Hickel, R. O. (1951). Experimental Investigation of Air-cooled Turbine Blades in Turbo-jet Engine. IX.—Evaluation of Durability of Non-critical Rotor Blades in Engine Operation. N.A.C.A. R.M. E51J10 (1951).Google Scholar
24. Smith, A. G. and Pearson, R. D. (1950). The Cooled Gas Turbine. Proc. I. Mech. E., Vol. 163 (1950).Google Scholar
25. A New Nimonic Development. (Extruded Blade Sections with Cooling Passages.) Metallurgia, Vol. 50, No. 301 (1954).Google Scholar
26. Destival, P. (1949). French Turbo-propeller and Turboreaction Engines. Journal of the Royal Aeronautical Society, Vol. 53, No. 458 (1949).CrossRefGoogle Scholar
27. Staniforth, R. (1951). Contribution to the Theory of Effusion Cooling of Gas Turbine Blades. Proc. 1. Mech. E., General Discussion on Heat Transfer (1951).Google Scholar
28. Andrews, S. J., Ogden, H. and Marshall, J. (1954). Some Experiments on an Effusion Cooled Turbine Nozzle Blade. Unpublished N.G.T.E. Note (1954).Google Scholar
29. Cohen, H. and Bayley, F. J. (1955). Heat Transfer Problems of Liquid-cooled Gas Turbine Blades. Proc. 1. Mech. E. (1955).Google Scholar
30. Brown, T. W. F. (1954). High-temperature Turbine Machinery for Marine Propulsion. 26th Thomas Lowe Gray Lecture. Proc. I. Mech. E. (1954).Google Scholar
31. Martin, B. W. and Cohen, H. (1954). Heat Transfer by Free Convection in an Open Thermosyphon Tube. British Journal of Applied Physics, Vol. 5 (1954).Google Scholar
32. Burke, E. and Kemeny, G. A. (1953). A Novel Cooling Method for Gas Turbines. A.S.M.E. Paper No. 53-A-180 (1953).Google Scholar
33. Arc-cast Molybdenum and Its Alloys. Brochure of Climax Molybdenum Co. (1955).Google Scholar
34. Properties and Use of Niafrax. Brochure of Carborundum Co. Ltd.Google Scholar
35. Shevlin, T. S. (1954). Journal of American Ceramics Society, 37, 3, 140 (1954).Google Scholar
36. Trent, E. M., Carter, A. and Bateman, J. (1950). Metallurgia, August 1950.Google Scholar
37. Schwartzkoff, P. and Kieffer, R. (1953). Refractory Hard Metals. Macmillan (1953).Google Scholar
38. Freche, J. C. and Diaginla, A. J. (1950). Heat-transfer and Operating Characteristics of Aluminum Forcedconvection and Stainless-steel Natural-convection Watercooled Single-stage Turbines. N.A.C.A. R.M. R50D03a (1950).Google Scholar