Two-dimensional compressible flow in conical mixed-flow compressors
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Stanitz, John D↗
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Tables of wing-aileron coefficients of oscillating air forces for two-dimensional supersonic flow
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WINGS - AIR FORCES↗
On a source-sink method for the solution of the Prandtl-Busemann iteration equations in two-dimensional compressible flow
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EQUATIONS - FLOW - PRANDTL & BUSEMANN COMPRESSIBLE↗
Two-dimensional compressible flow in centrifugal compressors with logarithmic-spiral blades
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COMPRESSORS - BLADES↗
Turbulent boundary-layer temperature recovery factors in two-dimensional supersonic flow
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BOUNDARY LAYER - PLATES TURBULENT↗
On the second-order tunnel-wall-constriction corrections in two-dimensional compressible flow
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WIND TUNNEL TESTS - CORRECTION, BOUNDARY↗
Two-dimensional transonic flow past airfoils
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2-DIMENSIONAL↗
Calculation of higher approximations for two-dimensional compressible flow by a simplified iteration process
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Braun, W H↗
Calculations on the Forces and Moments for an Oscillating Wing-aileron Combination in Two-dimensional Potential Flow at Sonic Speed
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Nelson, Herbert C↗
Two-dimensional shear flow in a 90 degrees elbow
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Kramer, James J↗
An Approximate Method for Determining the Displacement Effects and Viscous Drag of Laminar Boundary Layers in Two-dimensional Hypersonic Flow
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Bertram, Mitchel H↗
An application of the method of characteristics to two-dimensional transonic flows with detached shock waves
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FLOW, MIXED↗
Two-dimensional subsonic flow past elliptic cylinder by the variational method
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Rao, G V R↗
A calculation study of wing-aileron flutter in two degrees of freedom for two-dimensional supersonic flow
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Woolston, Donald S↗
Impingement of water droplets on a rectangular half body in a two-dimensional incompressible flow field
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Lewis, William↗
Theoretical loss relations for low-speed two-dimensional-cascade flow
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Lieblein, Seymour↗
Effect of Angle of Attack and Thickness on Aerodynamic Coefficients of a Rigid Wing Oscillating at Very Low Frequencies in Two-dimensional Supersonic Flow
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Malvestuto, Frank S , Jr↗
Theory of two-dimensional potential flow about arbitrary wing sections
Three general theories treating the potential flow about an arbitrary wing section are discussed in this report. The first theory treats the method of conformal transformation as laid down by Theodorsen and Garrick; the second is a generalization of Birnbaum's theory for moderately thick airfoils; the third is a general investigation of the complex velocity function with particular reference to the relations first discussed by F. Weinig.
Gebelein, H↗