The Calculation of Downwash Behind Supersonic Wings with an Application to Triangular Plan Forms
Download or Read eBook The Calculation of Downwash Behind Supersonic Wings with an Application to Triangular Plan Forms PDF written by Max A. Heaslet and published by . This book was released on 1948 with total page 726 pages. Available in PDF, EPUB and Kindle.
Author | : Max A. Heaslet |
Publisher | : |
Total Pages | : 726 |
Release | : 1948 |
ISBN-10 | : STANFORD:36105024795713 |
ISBN-13 | : |
Rating | : 4/5 (13 Downloads) |
Book Synopsis The Calculation of Downwash Behind Supersonic Wings with an Application to Triangular Plan Forms by : Max A. Heaslet
Book excerpt: A method is developed, consistent with the assumptions of small perturbation theory, which provides a means of determining for a known load distribution, the downwash behind a wing in supersonic flow. THe analysis is based upon the use of supersonic doublets which are distributed over the plan form and wake of the wing in a manner determined from the wing loading.