Hostname: page-component-7479d7b7d-68ccn Total loading time: 0 Render date: 2024-07-13T16:06:45.123Z Has data issue: false hasContentIssue false
  • English
  • Français

The History and Progress of Refuelling in Flight

Published online by Cambridge University Press:  28 July 2016

Alan Cobham  and
Marcus Langley
Get access Rights & Permissions [Opens in a new window]

Extract

My experimental work in flight refuelling goes back over a period of ten years, when I became interested in its possibilities as a means of removing the hazard' of a heavily loaded take-off. My idea was that an aircraft should have a normal and safe take-off, and that when it was comfortably in the air, it should receive its load of fuel, thus being given both an extended range and an increased1 pay-load.

In 1932, initial experiments were carried out on two D.H. 9's, and early in 1933, we continued experiments with a D.H.9 and a Handley Page W.iotransport machine.

Type
Research Article
Information
The Aeronautical Journal , Volume 44 , Issue 355 , July 1940 , pp. 557 - 603
Copyright
Copyright © Royal Aeronautical Society 1940

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. “Aerodynamics,” Lanchester, F. W., L.L.D., F.R.S., Hon.F.R.Ae.S. Prop. I, §164.Google Scholar
2. Journal R.Ae.S., Vol. XLII, 1938 : “The Effect of Wing Loading on the Design of Modern Aircraft,” Vessey, H. F., B.Sc, A.F.R.Ae.S.Google Scholar
3. “ Aircraft Engineering,” June, 1938: “ High Wing Loadings,” H. Belart, Dipl.Ing., A.F.R.Ae.S.Google Scholar
4. Engineering Journal (Aeronautical Section Reprint No. 8, August, 1938): “North Atlantic Air Service London—Montreal,” J. H. Parkin, M.E.I.C. (The Engineering Institute of Canada).Google Scholar
5. Air Annual of the British Empire, 1938 : “ Advantages Conferred by Optimum Wing Loading,” Atcherley, R. L. R..Google Scholar
6. Journal R.Ae.S., Vol. XXXVIII, 1934, page 477 : “ A Method of Comparing the Performances of Civil Aircraft,” Langley, M., M.I.Ae.E., A.M.Inst.N.A.CrossRefGoogle Scholar
7. A.P. 1208, “ Airworthiness Handbook for Civil Aircraft,” Design Leaflet F.l.Google Scholar
8. Journal R.Ae.S., Vol. XXXIX, 1935, page 1010 : “ The Developments and Reliability of the Modern Multi-Engine Air Liner (with Special Reference to Multi-Engine Airplanes after Engine Failure),” by Douglas, Donald W..Google Scholar
9. Journal R.Ae.S., Vol. XLI, 1937 : “ Notes on the Design of Aeroplanes for Attaining High Altitude,” Capt. Barnwell, F. S., B.Sc, F.R.Ae.S.Google Scholar
10. Journal R.Ae.S., Vol. XLI, 1937 : “ Recent Progress in the Design of Civil Flying Boats,” Gouge, A., B.Sc, F.R.Ae.S.Google Scholar
11. Journal R.Ae.S., Vol. XLI, 1937 : “ Trend of Air-Cooled Engines,” Fedden, A. H. R., M.B.E., M.I.A.E., M.S.A.E., F.R.Ae.S.Google Scholar
12. “Flight” (Aircraft Engineer Supplement), September 27th, 1934.Google Scholar
13. “Flight” (Aircraft Engineer Supplement), March 31st, 1938.Google Scholar
14. Journal of Aeronautical Sciences, Vol. 4, No. 3, January, 1937 : “ Integral Fuel Tanks for Airplanes,” Alter, Horace J..CrossRefGoogle Scholar
15. Journal R.Ae.S., December, 1938 : “ Engineering Aspects of Commercial High Altitude Flying,” Younger, John E., Ph.D., A.F.I.Ae.S.Google Scholar