Theoretical span load distributions and rolling moments for sideslipping wings of arbitrary plan form in incompressible flow
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Queijo, M J↗
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Results for “Load Distribution”
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A summary report on the effects of Mach number on the span load distribution on wings of several models
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Jessen, Henry, Jr↗
Two-dimensional Chord-wise Load Distributions at Transonic Speeds
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Lindsey, Walter F↗
Load Distribution over a Fuselage in Combination with a Swept Wing at Small Angles of Attack and Transonic Speeds
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White, Maurice D↗
Wing Load Distribution on a Swept Wing Airplane in Flight at Mach Numbers up to 1.11, and Comparison with Theory
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Rolls, L Stewart↗
Aerodynamics of Slender Bodies at Mach Number of 3.12 and Reynolds Numbers from 2 x 10(exp 6) to 15 x 10(exp 6) II : Aerodynamic Load Distributions of Series of Five Bodies Having Conical Noses and Cylindrical Afterbodies
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Jack, John R↗
Notes on damping in roll and load distributions in roll at high angles of attack and high subsonic speed
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Source record↗
The interference effects of a body on the spanwise load distributions of two 45 degrees sweptback wings of aspect ratio 8 from low-speed tests at a Reynolds number of 4 x 10(exp 6)
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Martina, Albert P↗
Aerodynamics of Slender Bodies at Mach Number of 3.12 and Reynolds Numbers from 2 x 10(exp 6) to 15 x 10(exp 6) V : Aerodynamic Load Distributions for a Series of Four Boattailed Bodies
Pressure distributions for a series of four boattailed bodies of revolution were obtained and compared with theory for a Mach number of 3.12, a Reynolds number range of 2 x 10 to 6th power to 14 x 10 to the 6th power, and angles of attack from zero to 9 degrees. Second-order theory adequately predicted the pressure distribution for regions free of the effects of cross-flow separation.
Moskowitz, Barry↗
Effects of spoiler ailerons on the aerodynamic load distribution over a 45 degree sweptback wing at Mach numbers from 0.60 to 1.03
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Hallissy, Joseph M , Jr↗
Load distributions on wings and wing-body combinations at high angles of attack and supersonic speeds
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Katzen, Elliott D↗
Load distributions associated with controls at supersonic speeds
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Czarnecki, K R↗
Air load distributions on a flapped wing resulting from leading-edge and trailing-edge blowing
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Mclemore, H Clyde↗
Investigation at Mach numbers from 0.80 to 1.43 of pressure and load distributions over a thin 45 degree sweptback highly tapered wing in combination with basic and indented bodies
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Fischetti, Thomas L↗
Flight measurements and calculations of wing loads and load distributions at subsonic, transonic, and supersonic speeds
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Malvestudo, Frank S↗
Aerodynamic Load Distribution on a 45 Degree Sweptback Wing with Leading-edge Chord-extensions at Transonic Speeds, Including Effects of a Spoiler-slot-deflector Aileron
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Schmeer, James W↗
An Analysis of Surface Pressures and Aerodynamic Load Distribution over the Swept Wing of the Douglas D-558-II Research Airplane at Mach Numbers from 0.73 to 1.73
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Taillon, Norman V↗
Aerodynamic Load Distribution over a 45 Degree Swept Wing Having a Spoiler-slot-deflector Aileron and Other Spoiler Ailerons for Mach Numbers from 0.60 to 1.03
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West, F E , Jr↗