Experimental Pressure Distributions Over Wing Tips at Mach Number 1.9
Author | : Harold Mirels |
Publisher | : |
Total Pages | : 28 |
Release | : 1949 |
ISBN-10 | : UOM:39015086432187 |
ISBN-13 | : |
Rating | : 4/5 (87 Downloads) |
Download or read book Experimental Pressure Distributions Over Wing Tips at Mach Number 1.9 written by Harold Mirels and published by . This book was released on 1949 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted at a Mach number of 1.90 to determine spanwise pressure distribution over a wing tip in a region influenced by a sharp subsonic trailing edge. The wing section was a symmetrical wedge of 5 degrees 43 minutes total included angle in the free-stream direction. The investigation was conducted over a range of angles of attack from -10 to 10 degrees at a Reynolds number of 3,400,000 per foot.