Calculation of the aerodynamic loading of flexible wings of arbitrary plan form and stiffness
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Diederich, Franklin W↗
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Low-speed investigation of the aerodynamic loads on the droop-nose flap of a wing with leading edge swept back 47.5 degrees and having symmetrical circular-arc airfoil sections at a Reynolds number of 4.3 x 10 (exp 6)
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Whittle, Edward F , Jr↗
Time histories of the aerodynamic loads on the vertical and horizontal tail surfaces of a jet-powered bomber airplane during sideslip maneuvers at approximately 20,000 feet
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Cooney, T V↗
Flight Measurements with the Douglas D-558-II (buaero No. 37974) Research Airplane : Measurements of the Distribution of the Aerodynamic Load Among the Wing, Fuselage, and Horizontal Tail at Mach Numbers up to 0.87
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Mayer, John P↗
The Effects of Camber and Twist on the Aerodynamic Loading and Stalling Characteristics of a Large-scale 45 Degree Swept-back Wing
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Hunton, Lynn W↗
Calculated aerodynamic loadings of M, W, and delta wings in incompressible flow
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Diederich, Franklin W↗
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↗
Aerodynamic Loading Characteristics of a Wing-fuselage Combination Having a Wing of 45 Degrees Sweepback Measured in the Langley 8-foot Transonic Tunnel
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Loving, Donald L↗
Aerodynamic Load Measurements over a Leading-edge Slat on a 40 Degree Sweptback Wing at Mach Numbers from 0.10 to 0.91
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Cahill, Jones F↗
A method for calculating the aerodynamic loading on wing-tip-tank combinations in subsonic flow
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Robinson, Samuel W , Jr↗
A simplified mathematical model for calculating aerodynamic loading and downwash for midwing wing-fuselage combinations with wings of arbitrary plan form
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Zlotnick, Martin↗
A study of the aerodynamic loads on sweptback wings at transonic speeds
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Williams, Claude V↗
Wind-tunnel Investigation of the Effects of a Fence and a Leading-edge Notch on the Aerodynamic Loading Characteristics in Pitch of a 45 Degree Sweptback Wing at High Subsonic Speeds
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Kuhn, Richard E↗
Flight Measurement of Aerodynamic Loads and Moments on an External Store Mounted Under the Wing of a Swept-wing Fighter-type Airplane
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O'Bryan, Thomas C↗
Transonic Flight Measurement of the Aerodynamic Load on the Extended Slat of the Douglas D-558-II Research Airplane
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Peele, James R↗
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↗
Aerodynamic load measurements and opening characteristics of automatic leading-edge slats on a 45 degree sweptback wing at transonic speeds
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Arabian, Donald D↗