Hostname: page-component-745bb68f8f-b6zl4 Total loading time: 0 Render date: 2025-01-14T11:20:44.114Z Has data issue: false hasContentIssue false
  • English
  • Français

Maximum Range of Hypersonic Ramjets

Published online by Cambridge University Press:  04 July 2016

J. H. Horlock
J. H. Horlock*
Affiliation:
University of Liverpool
Get access Rights & Permissions [Opens in a new window]

Extract

Recent studies of the performance of high-speed aircraft have emphasised the importance of engine-airframe integration. For example, Probert and Mallinson, and Bragg have pointed out the advantages of jet deflection in producing extra lift with little penalty in decreased thrust. Townend has drawn attention to producing thrust or lift on high-speed aircraft by external heat addition, and has calculated the effects on the range of the aircraft.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 68 , Issue 646 , October 1964 , pp. 699 - 702
Copyright
Copyright © Royal Aeronautical Society 1964

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.Probert, R. P. and Mallinson, D. H.Economics of Ramjets as Satellite Launchers. Journal of the Royal Aeronautical Society, Vol. 66, p. 357, June 1962.Google Scholar
2.Bragg, S.L. Aeronautical Quarterly, August 1963.Google Scholar
3.Townend, L. H. Effects of External Heat Addition on Supersonic Cruise Performance. Aeronautical Quarterly, August 1962.Google Scholar
4.Keenan, J. H. and Kaye, J.Gas Tables. John Wiley, 1948.Google Scholar
5.The Use of Jet Deflection to Extend the Cruise Range of a Supersonic Aircraft. N.G.T.E. Engine Research Note, 1958.Google Scholar
6.Pearson, H. Private communication, 1962.Google Scholar