One-dimensional Compressible Flow in Vaneless Diffusers of Radial- and Mixed-flow Centrifugal Compressors, Including Effects of Friction, Heat Transfer and Area Change
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Stanitz, John D↗
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Results for “compressible flows”
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General Consideration of Problems in Compressible Flow Using the Hodograph Method
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Chang, Chieh-Chien↗
Expressions for measuring the accuracy of approximate solutions to compressible flow through cascades of blades with examples of use
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Sinnette, John T↗
Studies on von Karman's similarity theory and its extension to compressible flows : a critical examination of similarity theory for incompressible flows
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Lin, C C↗
Linearized Potential Theory of Propeller Induction in a Compressible Flow
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Davidson, Robert E↗
Prediction of losses induced by angle of attack in cascades of sharp-nosed blades for incompressible and subsonic compressible flow
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Kramer, James J↗
A Compressible-flow Plotting Device and Its Application to Cascade Flows
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Wesphal, Willard R↗
Theoretical and Experimental Analysis of One-dimensional Compressible Flow in a Rotating Radial-inlet Impeller Channel
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Lieblein, Seymour↗
On the form of the turbulent skin-friction law and its extension to compressible flows
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Donaldson, Coleman Dup↗
Theoretical and experimental investigation of the effect of tunnel walls on the forces on an oscillating airfoil in two-dimensional subsonic compressible flow
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Runyan, Harry L↗
Analysis of two-dimensional compressible-flow loss characteristics downstream of turbomachine blade rows in terms of basic boundary-layer characteristics
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Stewart, Warner L↗
Laminar separation over a transpiration-cooled surface in compressible flow
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Morduchow, Morris↗
General Treatment of Compressible Flow in Ejectors and Example of Its Application to Problem of Effect of Ejector Addition on Thrust of Jet-propulsion Units
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Ellerbrock, Herman H , Jr↗
A theoretical and experimental study of wind-tunnel-wall effects on oscillating air forces for two-dimensional subsonic compressible flow
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Runyan, Harry L↗
Investigation of Compressible Flow Mixing Losses Obtained Downstream of a Blade Row
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Stewart, Warner L↗
Compressible-flow solutions for the actuator disk
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Delano, James B↗
Linearized compressible-flow theory for sonic flight speeds
The partial differential equation for the perturbation velocity potential is examined for free-stream Mach numbers close to and equal to one. It is found that, under the assumptions of linearized theory, solutions can be found consistent with the theory for lifting-surface problems both in stationary three-dimensional flow and in unsteady two-dimensional flow. Several examples are solved including a three dimensional swept-back wing and two dimensional harmonically-oscillating wing, both for a free stream Mach number equal to one. Momentum relations for the evaluation of wave and vortex drag are also discussed. (author)
Heaslet, Max A↗
Approximate formulas for the computation of turbulent boundary-layer momentum thicknesses in compressible flows
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Tetervin, Neal↗