Wind Tunnel Investigation Of Effect Of Sweep On Rolling Derivatives At Angles Of Attack Up To 13 Degrees And At High Subsonic Mach Numbers Including A Semiempirical Method Of Estimating The Rolling Derivatives
Download Wind Tunnel Investigation Of Effect Of Sweep On Rolling Derivatives At Angles Of Attack Up To 13 Degrees And At High Subsonic Mach Numbers Including A Semiempirical Method Of Estimating The Rolling Derivatives full books in PDF, epub, and Kindle. Read online free Wind Tunnel Investigation Of Effect Of Sweep On Rolling Derivatives At Angles Of Attack Up To 13 Degrees And At High Subsonic Mach Numbers Including A Semiempirical Method Of Estimating The Rolling Derivatives ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
| Author | : James W. Wiggins |
| Publisher | : |
| Total Pages | : 56 |
| Release | : 1954 |
| Genre | : Airplanes |
| ISBN | : |
An investigation was performed in the Langley high-speed 7- by 10-foot tunnel in order to determine the rolling derivatives for swept-wing-body configurations at angles of attack from 0 degrees to 13 degrees and at high subsonic Mach numbers. The wings had sweep angles of 3.6 degrees, 32.6 degrees, 45 degrees, and 60 degrees at the quarter-chord line, an aspect ratio of 4, a taper ratio of 0.6, and an NACA 65A006 airfoil section parallel to the free stream. The results indicate a reduction in the damping-in-roll derivative at the higher test angles of attack. Of the wings tested, instability of the damping-in-roll derivative was experienced over the largest ranges of angle of attack and Mach number for the 32.6 sweptback wing.
| Author | : James W. Wiggins |
| Publisher | : |
| Total Pages | : 47 |
| Release | : 1958 |
| Genre | : |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 524 |
| Release | : 1953 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 716 |
| Release | : 1956 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : National Research Council Canada |
| Publisher | : |
| Total Pages | : 762 |
| Release | : 1960 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : Defense Documentation Center (U.S.) |
| Publisher | : |
| Total Pages | : 308 |
| Release | : 1960 |
| Genre | : Science |
| ISBN | : |
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 1516 |
| Release | : 1958 |
| Genre | : Aeronautics |
| ISBN | : |
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
| Author | : Clifford J. Moore |
| Publisher | : |
| Total Pages | : 492 |
| Release | : 1970 |
| Genre | : |
| ISBN | : |
| Author | : United States. National Aeronautics and Space Administration |
| Publisher | : |
| Total Pages | : 506 |
| Release | : 1970 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : Royal Aeronautical Society |
| Publisher | : |
| Total Pages | : 1272 |
| Release | : 1958 |
| Genre | : Aeronautics |
| ISBN | : |
