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| Author | : William Solomon |
| Publisher | : |
| Total Pages | : 44 |
| Release | : 1953 |
| Genre | : Aerodynamics, Transonic |
| ISBN | : |
| Author | : William Solomon |
| Publisher | : |
| Total Pages | : 36 |
| Release | : 1953 |
| Genre | : |
| ISBN | : |
| Author | : Joseph M. Hallissy |
| Publisher | : |
| Total Pages | : 38 |
| Release | : 1953 |
| Genre | : |
| ISBN | : |
| Author | : Harold L. Robinson |
| Publisher | : |
| Total Pages | : 94 |
| Release | : 1954 |
| Genre | : Aerodynamic load |
| ISBN | : |
| Author | : Earl D. Knechtel |
| Publisher | : |
| Total Pages | : 32 |
| Release | : 1957 |
| Genre | : Airplanes |
| ISBN | : |
An investigation was conducted to determine the effects of wing-tip droop on the longitudinal stability characteristics of a 53 and a 63 degree sweptback wing-body combination. Both models were tested with flat and abruptly drooped wing tips. The 63 degree wing was also tested with a curved drooped tip. In addition, the combined effects of wing fences and extended leading-edge flaps were investigated. The results showed that abrupt droop of the outer 40 percent of the basic 53 degree wing improved the stability characteristics of the model. For the 63 degree swept wing, curved droop caused slight beneficial effects on the stability, whereas abrupt droop caused adverse effects. In general, the most favorable stability characteristics were obtained for either flat or abruptly drooped wings with fences and extended leading-edge flaps.
| Author | : Albert G. Few |
| Publisher | : |
| Total Pages | : 80 |
| Release | : 1954 |
| Genre | : Airplanes |
| ISBN | : |
The drag due to lift increases with increasing sweep through the Mach number range. Some increase in bag due to lift is evident decrease in taper ratio for wings having 300of sweep through most of the speed range.
| Author | : George L. Pratt |
| Publisher | : |
| Total Pages | : 110 |
| Release | : 1952 |
| Genre | : Airplanes |
| ISBN | : |
| Author | : Jacob H. Lichtenstein |
| Publisher | : |
| Total Pages | : 34 |
| Release | : 1951 |
| Genre | : Airplanes |
| ISBN | : |
Wind-tunnel results are presented to show the effect of changes in horizontal-tail location on the low-speed static longitudinal stability and steady-state rotary damping in pitch for a complete model with wing and tail surfaces having the quarter-chord lines swept back 45 degrees.
| Author | : Stanley H. Spooner |
| Publisher | : |
| Total Pages | : 28 |
| Release | : 1956 |
| Genre | : Aerodynamics, Transonic |
| ISBN | : |
The combined effects of wing taper ratio and low horizontal-tail position on the static longitudinal stability of a 45 degree sweptback wing-body combination with an aspect ratio of approximately 4 have been investigated for a range of Mach numbers from 0.8 to 1.2 in the Langley 8-foot transonic pressure tunnel.
| Author | : William B. Kemp |
| Publisher | : |
| Total Pages | : 32 |
| Release | : 1953 |
| Genre | : Airplanes |
| ISBN | : |
