Some Theoretical Characteristics Of Trapezoidal Wings In Supersonic Flow And A Comparison Of Several Wing Flap Combinations
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Some Theoretical Characteristics of Trapezoidal Wings in Supersonic Flow and a Comparison of Several Wing-flap Combinations
Author | : Robert O. Piland |
Publisher | : |
Total Pages | : 32 |
Release | : 1951 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
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The theoretical lift and pitching moment due to angle of attack and pitching and the lateral force and yawing moment due to rolling of a trapezoidal wing are derived. The equations are applicable when the inboard Mach line from a leading-edge tip intersects the trailing edge and the outboard Mach line lies ahead of the side edge. When the side edges are raked in, the former condition is sufficient. A comparison based on theoretical expressions of the lift and rolling effectiveness for half-delta tip (point forward) and trailing-edge flaps on various plan forms is made.
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