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| Author | : A. J. Eggers |
| Publisher | : |
| Total Pages | : 264 |
| Release | : 1950 |
| Genre | : Aerofoils |
| ISBN | : |
| Author | : John C. Evvard |
| Publisher | : |
| Total Pages | : 32 |
| Release | : 1950 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 620 |
| Release | : 1945 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 996 |
| Release | : 1950 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : |
| Release | : 1955 |
| Genre | : Aeronautics |
| ISBN | : |
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
| Author | : G. N. Ward |
| Publisher | : Cambridge University Press |
| Total Pages | : 261 |
| Release | : 2016-02-25 |
| Genre | : Mathematics |
| ISBN | : 1316601897 |
Originally published in 1955, this book is devoted exclusively to the problems involved in solving the non-linear equations of motion for compressible fluids.
| Author | : |
| Publisher | : CUP Archive |
| Total Pages | : 268 |
| Release | : |
| Genre | : |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 234 |
| Release | : 1951 |
| Genre | : Science |
| ISBN | : |
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 958 |
| Release | : 1955 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : Elmer A. Horton |
| Publisher | : |
| Total Pages | : 678 |
| Release | : 1950 |
| Genre | : Airplanes |
| ISBN | : |
An investigation was made to determine the effects of boundary-layer control on the landing performance characteristics of a liaison type of airplane having a payload of 1500 pounds and a flight duration of 5 hours. The aspect ratio was varied from 5 to 15, the wing span from 30 to 100 feet, and the brake horsepower from 300 to 1200. The use of boundary-layer control caused reduction in total landing distance (25 to 40 percent), ground-run distance, gliding speed, and stalling speed whereas sinking speed was increased only slightly.
