Two-Dimensional Gas Jets

[+] Author and Article Information
M. J. Cohen

Northampton College of Advanced Technology, London, England

J. Appl. Mech 27(4), 603-608 (Dec 01, 1960) (6 pages) doi:10.1115/1.3644067 History: Received October 17, 1958; Revised November 19, 1959; Online September 16, 2011


A method is described for solving certain problems of subsonic aerodynamic design where flow boundaries in the physical plane are required to have specific dynamic characteristics. The method is tested on two type-problems with known exact solutions: the two-dimensional gas jet and the flow in the neighborhood of stagnation points. It has been found to give the solution with a degree of accuracy acceptable for practical design.

Copyright © 1960 by ASME
Your Session has timed out. Please sign back in to continue.





Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In