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| Author | : Paul G. Fournier |
| Publisher | : |
| Total Pages | : 34 |
| Release | : 1953 |
| Genre | : Aerodynamics, Supersonic |
| ISBN | : |
| Author | : James W. Wiggins |
| Publisher | : |
| Total Pages | : 25 |
| Release | : 1957 |
| Genre | : |
| ISBN | : |
| Author | : Arthur Henderson |
| Publisher | : |
| Total Pages | : 94 |
| Release | : 1956 |
| Genre | : Aerodynamics, Supersonic |
| ISBN | : |
An investigation to determine the static longitudinal and lateral stability characteristics of a 1/62-scale model of the X-1E has been conducted in the Langley 9-inch supersonic tunnel. Tests were made at Mach numbers of 1.62, 1.94, 2.22, 2.40, and 2.62 on the wing-body, wing-body-vertical-tail, and complete model configurations. Detailed analysis of the test results has not been made.
| Author | : Richard E. Kuhn |
| Publisher | : |
| Total Pages | : 30 |
| Release | : 1952 |
| Genre | : Airplanes |
| ISBN | : |
An investigation has been made in the Langley high-speed 7- by 10-foot tunnel to determine the effect of sweep on the static lateral stability characteristics of wing-fuselage combinations having wings of aspect ratio 4 and taper ratio 0.6 at high subsonic speeds.
| Author | : James W. Wiggins |
| Publisher | : |
| Total Pages | : 0 |
| Release | : 1957 |
| Genre | : |
| ISBN | : |
| Author | : James W. Wiggins |
| Publisher | : |
| Total Pages | : 26 |
| Release | : 1953 |
| Genre | : |
| ISBN | : |
| Author | : William A. Newsom |
| Publisher | : |
| Total Pages | : 104 |
| Release | : 1959 |
| Genre | : Aerodynamics |
| ISBN | : |
| Author | : Isidore G. Recant |
| Publisher | : |
| Total Pages | : 36 |
| Release | : 1942 |
| Genre | : Airplanes |
| ISBN | : |
Combinations of an NACA 23012 tapered wing and a circular fuselage having a wedge-shaped rear were tested in the NACA 7- by 10-foot wind tunnel to determine the effect of wing-fuselage interference on the lateral-stability of wing-fuselage interference on the lateral-stability characteristics. The model configurations represented a high-wing, a mid-wing, and a low-wing monoplane. For each configuration, tests were made with a partial-span split flap neutral and deflected 60 degrees and with and without a vertical tail. Tests of the fuselage alone and of the fuselage with the vertical tail were also made.
| Author | : United States. National Aeronautics and Space Administration |
| Publisher | : |
| Total Pages | : 498 |
| Release | : 1958 |
| Genre | : |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 818 |
| Release | : 1954 |
| Genre | : Aeronautics |
| ISBN | : |
