Hostname: page-component-848d4c4894-cjp7w Total loading time: 0 Render date: 2024-07-07T22:30:15.512Z Has data issue: false hasContentIssue false
  • English
  • Français

The Momentum Equation for a Static Hovercraft at Zero Incidence

Published online by Cambridge University Press:  04 July 2016

S. M. Fraser
S. M. Fraser*
Affiliation:
University of Strathclyde
Get access Rights & Permissions [Opens in a new window]

Extract

The technical note by Dr. Alexander implies that hovercraft jet performance might be better than simple theory predicts for values of 1/x greater than 4. The experimental points used to compare with theory were obtained at the beginning of hovercraft development, but subsequently a number of British and American reports have been issued whose data can be interpreted to give points for comparison with theory. These results show that the simple theory overestimates the performance of the jet.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 71 , Issue 681 , September 1967 , pp. 651 - 652
Copyright
Copyright © Royal Aeronautical Society 1967

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.Alexander, A. J.The Momentum Equation—for a Static Hovercraft at Zero Incidence. Journal of the Royal Aero nautical Society, Vol 70, p 363, February 1966.Google Scholar
2.Chaplin, H. R. Effect of Jet Mixing on the Annular Jet. DTMB Aero Report No 953, February 1959.Google Scholar
3.Shen, S. F.Fundamentals of the Stability of Peripheral Jet Vehicles. Systems Engineering Division of Pneumo- dynamics Corporation, Bethesda, Md, Vol 3, November 1960.Google Scholar
4.Hsu, C. C. Viscous Effects on Balanced Jets in Ground Proximity. Hydronautics Inc, Laurel, Md, Tech Report No 241-1, October 1963.Google Scholar
5.Burgess, A. J. A Two-Dimensional Static Stability Theory for an ACV with Central Stability Jet. Univ of Southampton AASU Tech Note 256.Google Scholar
6.Barratt, M. J. Simple Curtain Theory and the “Split“ Jet. HDL Hythe, 1961 (unpublished).Google Scholar