Hostname: page-component-848d4c4894-pjpqr Total loading time: 0 Render date: 2024-06-28T21:33:09.695Z Has data issue: false hasContentIssue false
  • English
  • Français

Configurations for High Supersonic Speeds Derived from Simple Shock-waves and Expansions

Published online by Cambridge University Press:  04 July 2016

J. W. Flower
J. W. Flower*
Affiliation:
Aeronautical Engineering, University of Bristol
Get access Rights & Permissions [Opens in a new window]

Summary

The Nonweiler method of designing delta wings (caret wings) to have plane shocks on the lower surface is extended to the design of upper surfaces. Cambered and shock-free surfaces are also deduced, and methods of design for complete configurations suggested.

An important point is that all surfaces are of single curvature.

Type
Research Article
Information
The Aeronautical Journal , Volume 67 , Issue 629 , May 1963 , pp. 287 - 290
Copyright
Copyright © Royal Aeronautical Society 1963

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.)