Wind-tunnel Investigation of Damping in Roll at Supersonic Speeds of Triangular Wings at Angles of Attack
Author | : Russell W. McDearmon |
Publisher | : |
Total Pages | : 42 |
Release | : 1956 |
ISBN-10 | : UOM:39015086490169 |
ISBN-13 | : |
Rating | : 4/5 (69 Downloads) |
Download or read book Wind-tunnel Investigation of Damping in Roll at Supersonic Speeds of Triangular Wings at Angles of Attack written by Russell W. McDearmon and published by . This book was released on 1956 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: Experimental values of the damping in roll of three triangular wings have been obtained at Mach numbers of 1.62, 1.94, 2.22, 2.41, and 2.62 over a range of angle of attack from approximately 0 to 13 degrees. The aspect ratios of the wings were 1.46, 2.31, and 3.35.