Generalized conical-flow fields in supersonic wing theory
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WINGS, COMPLETE - SWEEP↗
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Results for “Wing loading”
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Use of Two-dimensional Data in Estimating Loads on a 45 Degree Sweptback Wing with Slats and Partial-span Flaps
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Hunton, Lynn W↗
A Method for Calculating the Subsonic Steady-state Loading on an Airplane with a Wing of Arbitrary Plan Form and Stiffness
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Gray, W L↗
A theoretical estimate of the effects of compressibility on the performance of a helicopter rotor in various flight conditions
The effects of compressibility arising from high-tip-speed operation on the flapping, thrust, and power of a helicopter rotor in forward speed are investigated for a particular set of airfoil characteristics. Tip-speed ratios ranging from 0.2 to 0.5 were covered at several tip-speed values.
WINGS, ROTATING - THEORY↗
Experimental Pressure Distributions over Wing Tips at Mach Number 1.9 I : Wing Tip with Subsonic Leading Edge
An investigation was conducted at a Mach number of 1.91 to determine spanwise pressure distribution over a wing tip in a region influenced by a sharp subsonic leading edge swept back at 70 degrees. Except for pressure distribution on the top surface in the immediate vicinity of the subsonic leading edge, the maximum difference between linearized theory and experimental data was 2 1/2 percent (of free-stream dynamic pressure) for angles of attack up to 4 degrees and 7 percent for angles of attack up to 8 degrees. Pressures on the top surface nearest the subsonic edge indicated local expansions beyond values predicted by linearized theory.
FLOW, SUPERSONIC↗
Chordwise and Spanwise Loadings Measured at a Large Triangular Wing Having an Aspect Ratio of 2 and a Thin, Subsonic-type Airfoil Section
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Graham, David↗
Aerodynamic Study of a Wing-fuselage Combination Employing a Wing Swept Back 63 Degrees : Characteristics at Supersonic Speeds of a Model with the Wing Twisted and Cambered for Uniform Load
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Hall, Charles F↗
Aerodynamic Study of a Wing-fuselage Combination Employing a Wing Swept Back 63 Degrees : Effect of Reynolds Number at Supersonic Mach Numbers on the Longitudinal Characteristics of a Wing Twisted and Cambered for Uniform Load
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Heitmeyer, John C↗
Calculated aerodynamic loadings of M, W, and delta wings in incompressible flow
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Diederich, Franklin W↗
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↗
The effects of wind incidence on the aerodynamic loading characteristics of a sweptback wing-body combination at transonic speeds
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Robinson, Harold L↗
Effects of wing-fuselage flow fields on missile loads at subsonic speeds
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Alford, William J , Jr↗
Investigation at transonic speeds of the loading over a 45 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2, and NACA 65A004 airfoil sections
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Runckel, Jack F↗
Horizontal-tail Parameters as Determined from Flight-test Tail Loads on a Flexible Swept-wing Jet Bomber
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Aiken, William S , Jr↗
Experimental Study and Analysis of Loading and Pressure Distributions on Delta Wings Due to Thickness and to Angle of Attack at Supersonic Speeds
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Boatright, William B↗
Investigation at Transonic Speeds of Loading over a 30 Degree Sweptback Wing of Aspect Ratio 3, Taper Ratio 0.2, and NACA 65A004 Airfoil Section Mounted on a Body
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Arabian, Donald D↗
Steady loads due to jet interference on wings, tails, and fuselages at transonic speeds
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Swihart, John M↗
Frequency of occurrence of critical gust loads on overloaded airplanes
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LOADS, GUST↗