Effects of High-lift and Stall-control Devices, Fuselage, and Horizontal Tail on a Wing Swept Back 42 Degrees at the Leading Edge and Having Symmetrical Circular-arc Airfoil Sections at a Reynolds Number of 6.9 X (10)6
| Author | : Robert L. Woods |
| Publisher | : |
| Total Pages | : 42 |
| Release | : 1949 |
| ISBN-10 | : OCLC:1109695489 |
| ISBN-13 | : |
| Rating | : 4/5 (89 Downloads) |
Book Synopsis Effects of High-lift and Stall-control Devices, Fuselage, and Horizontal Tail on a Wing Swept Back 42 Degrees at the Leading Edge and Having Symmetrical Circular-arc Airfoil Sections at a Reynolds Number of 6.9 X (10)6 by : Robert L. Woods
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