Effects of Mach Number Up to 0.34 and Reynolds Number Up to 8 X 10 6 on the Maximum Lift Coefficient of a Wing of NACA 66-series Airfoil Sections
| Author | : G. Chester Furlong |
| Publisher | : |
| Total Pages | : 43 |
| Release | : 1950 |
| ISBN-10 | : OCLC:249302242 |
| ISBN-13 | : |
| Rating | : 4/5 ( Downloads) |
Book Synopsis Effects of Mach Number Up to 0.34 and Reynolds Number Up to 8 X 10 6 on the Maximum Lift Coefficient of a Wing of NACA 66-series Airfoil Sections by : G. Chester Furlong
Download or read book Effects of Mach Number Up to 0.34 and Reynolds Number Up to 8 X 10 6 on the Maximum Lift Coefficient of a Wing of NACA 66-series Airfoil Sections written by G. Chester Furlong and published by . This book was released on 1950 with total page 43 pages. Available in PDF, EPUB and Kindle. Book excerpt: