Hostname: page-component-848d4c4894-hfldf Total loading time: 0 Render date: 2024-05-17T08:43:37.618Z Has data issue: false hasContentIssue false
  • English
  • Français

The Pressure Distribution on a Wing with a Subsonic Leading Edge in the Presence of Anti-symmetric Body Shaping

Published online by Cambridge University Press:  07 June 2016

J. G. Jones
J. G. Jones*
Affiliation:
Royal Aircraft Establishment, Bedford
Get access

Summary

The pressure distribution on the wing of a centrally mounted wingbody combination due to anti-symmetrical body shaping (with respect to the wing plane) can be calculated in the case where the wing leading edge is supersonic by using the fact that the upper and lower halves of the flow field are independent and that each half can be treated by quasi-cylinder theory. When the leading edge is subsonic the anti-symmetric body shaping produces flow round the leading edge. This paper is concerned with wing pressure distributions including the effect of this flow round the leading edge.

Type
Research Article
Information
Aeronautical Quarterly , Volume 11 , Issue 1 , February 1960 , pp. 51 - 70
Copyright
Copyright © Royal Aeronautical Society. 1960

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. Nielsen, J. N. Quasi-Cylindrical Theory of Wing-Body Interference at Supersonic Speeds and Comparison with Experiment. N.A.C.A. Report 1252, 1955.Google Scholar
2. Evvard, J. C. Use of Source Distributions for Evaluating Theoretical Aerodynamics of Thin Finite Wings at Supersonic Speeds. N.A.C.A. Report 951, 1950.Google Scholar
3. Robinson, A. and Laurmann, J. A, Wing Theory. Cambridge University Press, 1956.Google Scholar
4. Donovan, A. F. and Lawrence, H. R. High Speed Aerodynamics and Jet Propulsion. Vol. VII. Aerodynamic Components of Aircraft at High Speed. Oxford University Press, 1957.Google Scholar
5. Nielsen, J. N. Tables of Characteristic Functions for Solving Boundary-Value Problems of the Wave Equation. N.A.C.A. T.N. 3873, 1957.Google Scholar