Hostname: page-component-7479d7b7d-rvbq7 Total loading time: 0 Render date: 2024-07-13T06:26:18.279Z Has data issue: false hasContentIssue false
  • English
  • Français

Theory of an Accelerated Slender Supersonic Aerofoil

Published online by Cambridge University Press:  07 June 2016

Geoffrey L. Sewell
Geoffrey L. Sewell*
Affiliation:
University College, Hull
Get access

Summary

The problem of a uniformly accelerated slender supersonic aerofoil is solved in this paper by a perturbation method for the cases when the acceleration is small. Full account is taken of the effect of the acceleration on the form of the shock line.

Type
Research Article
Information
Aeronautical Quarterly , Volume 5 , Issue 1 , May 1954 , pp. 52 - 54
Copyright
Copyright © Royal Aeronautical Society. 1954

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

Sewell, G. L. (1950). Theory of an Oscillating Supersonic Aerofoil. Aeronautical Quarterly, May 1950.Google Scholar