A method recently developed for determining the steady flow of a nonviscous compressible fluid along a relative stream surface between adjacent blades in a turbomachine was applied to investigate the...
A general theory of steady three-dimensional flow of a nonviscous fluid in subsonic and supersonic turbomachines having arbitrary hub and casing shapes and a finite number of blades is presented, The...
General differentiation formulas for successive derivatives of a function are obtained in terms of the values of the function at unequally spaced arguments and the corresponding distances between the...
Wu, Chung-Hua, Brown, Curtis A.
A method of obtaining the flow of a nonviscous compressible fluid past arbitrary compressor or turbine blades between two neighboring surfaces of revolution is presented. The equations of continuity...
A general steady through-flow theory of nonviscous fluid in turbomachines: of arbitrary hub- and casing-wall shapes with subsonic or supersonic velocity is presented. The theory is applicable to both...
James J. Kramer, Vasily D. Prian, Chung-Hua Wu
A method for the solution of the incompressible nonviscous flow through a centrifugal impeller, including the inlet region, is presented. Several numerical solutions are obtained for four weight...
Subsonic flow of air through a single-stage and a seven-stage compressor (1953)
A method recently developed for solving the steady flow of a conviscous compressible fluid along a relative stream surface between two adjacent blades in a turbomachine is applied to investigate the...
Chung-Hua Wu, Curtis A. Brown, Vasily D. Prian
A method is presented to obtain a relatively quick approximate determination of the detailed subsonic flow of a nonviscous fluid past arbitrary turbomachine blades. The governing equations are...
Analysis of flow in a subsonic mixed-flow impeller (1952)
Chung-Hua Wu, Curtis A. Brown, Eleanor L. Costilow
A method recently developed for determining the steady flow of a nonviscous compressible fluid along a relative stream surface extending from hub to casing between two adjacent blades in a...
A general theory of steady three-dimensional flow of a nonviscous fluid in subsonic and supersonic turbomachines having arbitrary hub and casing shapes and a finite number of blades is presented. The...
A method of obtaining the flow of a nonviscous compressible fluid past arbitrary compressor or turbine blades between two neighboring surfaces revolution is presented. The equations of continuity and...
A rapid method for designing turbomachine blades of a given turning and desirable blade-thickness distribution for a compressible nonviscous fluid flow along an arbitrary stream filament of...
Chung-Hua Wu, Eleanor L. Costilow
Analysis of the supersonic flow in two two-dimensional high-solidity cascades and in a partly supersonic symmetrical nozzle shows that there is, in general, significant deviation of the mean...
Survey of available information on internal flow losses through axial turbomachines (1951)
No Abstract Available
Chung-Hua Wu, John T. Sinnette, Robert E. Forrette
An analysis was made of the effect at design condition of inlet hub-tip-radius ratio and mass flow per unit frontal area on the allowable rotor-tip speed, pressure ratio, and power input per unit...
General differentiation formulas for successive derivatives of a function are obtained in terms of the values of the function at unequally spaced arguments and the corresponding distances between the...
Application of radial-equilibrium condition to axial-flow compressor and turbine design (1949)
Chung-Hua Wu, Lincoln Wolfenstein
Basic general equations governing the three-dimensional compressible flow of gas through a compressor or a turbine are given in terms of velocity components, total enthalpy, and entropy. These...