Hostname: page-component-78c5997874-dh8gc Total loading time: 0 Render date: 2024-11-03T02:42:33.665Z Has data issue: false hasContentIssue false

Power Installations

Published online by Cambridge University Press:  28 July 2016

Extract

Never, at any time since the Wright Brothers made their first flight have the means of propulsion exercised a more dominant influence over the shape of aircraft or the shape of things to come, nor can it have been so difficult to forecast the form resulting from that influence. It has been a platitude for some time past to say that aircraft and engine design are mutually interdependent: now it is more than a platitude, it is a fact, and one to which we have not yet grown accustomed.

That power installations can no longer be procured “off the peg” is to-day an article of faith which is generally professed: what is rarer is an appreciation of the implications of this state of affairs. Pursued to its logical conclusion, the implication is that a new aircraft and its means of propulsion should originate in the same brain, and be designed, developed and manufactured under the guidance of that brain.

Type
Morning Session
Copyright
Copyright © Royal Aeronautical Society 1947

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. “Aircraft Engine Oil Cooling,” by Nixon, F., Esq., B.Sc., F.R.Ae.S., Journal of the R.Ae.S., March 1946.Google Scholar
2. “Cold Weather Operations,” by Dyment, J. T., Trans-Canada Air Lines report, No. 205-1-1, December 1941.Google Scholar
3. “Development of Thermal Ice-Prevention Equipment for the B-24D Airplane,” by Alan Jones, R. and Rodert, Lewis A., N.A.C.A. report, February 1943. (R.D.T.I(c)/363).Google Scholar
4. “German De-icing Technique” R.T.P. Translation No. 2,516 issued by the M.A.P.Google Scholar
5. “Heat anti-icing on PBY-5,” Field Service Bulletin of the Consolidated Vultee Aircraft Corporation.Google Scholar
6. “Hot Air De-icing—Heat transfer in the double Skin,” by the Staff of Ditton Laboratory, R.A.E. Technical Note No. S.M.E. 208, January 1944.Google Scholar
7. “Investigation of Wing De-icing by means of Hot Air,” by Hales, K. C. and Mann, G., R.A.E., Technical Note No. SME 255 and SME 206 (Revised) July 1944.Google Scholar
8. “Jet Propulsion,” by MajorHalford, F. B., F.R.Ae.S., M.S.A.E., Journal of the Royal Society of Arts, 16th August 1946.Google Scholar
9. “Note on Heat Exchangers for Wing Heating,” by Mr.Hardy, J. K., R.A.E. Note, February 1944.Google Scholar
10. “Present Achievements and Future Developments in Aircraft Gas Turbine Engines,” by Samaras, D. G., The Engineering Journal, July 1946.Google Scholar
11. “Prevention of Ice Formation on Military Aircraft,” by Anders, Karl, M.A.P. Translation 1249.Google Scholar
12. “Protection of Aircraft against Ice,” by Hardy, J. K., R.A.E.Google Scholar
13. “Enemy Aircraft: Ju 88, Wing De-icing System,” R.A.E. Technical Note No. EA 14/53 (June 1944).Google Scholar
14. “Report on Temperature Measurements on the Wing of a HE.177 with Hot Air De-icing System,” R.T.P. Translation No. 2533 issued by the M.A.P.Google Scholar
15. “Survey of Anti-icing Equipment,” Chandler, H. C. Jnr., N.A.C.A. Report (A.R.C. 5826), May 1942.Google Scholar
16. “Tests of a Merlin engine exhaust gas heat exchanger for aircraft thermal de-icing system,” by E. P. Hawthorne, B.A., F/O. Zaporski, B., Inz.Mech., and Brown, G., B.Sc., R.A.E Technical Note No. Eng.275, March 1944.Google Scholar
17. “The Airplane Icing Problem and its Alleviation through Research,” by Jones, Alan R., N.A.C.A.Google Scholar
18. “The Application of Jet Propulsion to Military Aircraft,” by Carter, W. G., F.R.Ae.S., Journal of the Royal Aeronautical Society, May 1946.Google Scholar
19. “The Application of the Gas Turbine in its Forms to the Field of Commercial Aviation,” by Clarkson, R. M., A.C.G.I., B.Sc., F.R.Ae.S., Journal of the R.Ae.S., May 1946.Google Scholar
20. “The Application of the Gas Turbine to Aircraft Propulsion,” by Dr.Hooker, S. G., B.Sc., D.I.C., D.Phil., A.F.R.Ae.S., Journal of the R.Ae.S., May 1946.Google Scholar
21. “The Future Scope of Propellers,” by Fairhurst, L. G., A.M.I.Mech.E., Journal of the R.Ae.S., December 1945.Google Scholar
22. “The processes of ice formation on Aircraft and methods of their prevention,” by Lebedev, N. B., R.T.P. Translation No. 1253, issued by the M.A.P.Google Scholar
23. “Turbine Compounding of the Piston Aeroengine,“ by Dr.Ricardo, H. R., F.R.S., F.R.Ae.S., Journal of the R.Ae.S., May 1946.Google Scholar
24. “Report on the Development and Application of Heated Wings,” U.S. Army Air Forces technical report circulated by R.T.P./T.I.B., M.A.P.Google Scholar