Effect of Wing Flexibility on the Damping in Roll of a Notched Delta Wing Body Combination Between Mach Numbers 0.6 and Approximately 2.2 as Determined with Rocket-propelled Models
| Author | : William M. Bland |
| Publisher | : |
| Total Pages | : 20 |
| Release | : 1954 |
| ISBN-10 | : OCLC:1109516006 |
| ISBN-13 | : |
| Rating | : 4/5 (06 Downloads) |
Book Synopsis Effect of Wing Flexibility on the Damping in Roll of a Notched Delta Wing Body Combination Between Mach Numbers 0.6 and Approximately 2.2 as Determined with Rocket-propelled Models by : William M. Bland
Download or read book Effect of Wing Flexibility on the Damping in Roll of a Notched Delta Wing Body Combination Between Mach Numbers 0.6 and Approximately 2.2 as Determined with Rocket-propelled Models written by William M. Bland and published by . This book was released on 1954 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
