Box 3
Contains 87 Results:
A general through-flow theory of fluid flow with subsonic or supersonic velocity in turbomachines of arbitrary hub and casing shapes,
by Chung-Hua Wu, National Advisory Committee for Aeronautics, Washington, D.C.(Technical note 2302), March 1951
The collection consists of reports and papers on the subjects of pumps, turbines, fans, metering and flow (hydraulics).
Flow through cascades in tandem,
by William E. Spraglin, National Advisory Committee for Aeronautics, Washington, D.C.(Technical note 2393), June 1951
The collection consists of reports and papers on the subjects of pumps, turbines, fans, metering and flow (hydraulics).
Axisymmetric supersonic flow in rotating impellers,
by Arthur W. Goldstein, National Advisory Committee for Aeronautics, Washington, D.C. (Technical note 2388), June 1951
The collection consists of reports and papers on the subjects of pumps, turbines, fans, metering and flow (hydraulics).
Possible application of blade boundary-layer control to improvement of design and off-design performance of axial-flow turbomachines,
by John T. Sinette, Jr., and George R. Costello, National Advisory Committee for Aeronautics, Washington, D.C. (Technical note 2371), May 1951
The collection consists of reports and papers on the subjects of pumps, turbines, fans, metering and flow (hydraulics).
Comparison of low-speed rotor and cascade performance for medium-camber NACA 65- (C10A10) 10 compressor-blade sections over a wide range of rotor blade-setting angles at solidities of 1.0 and 0.5,
by George C. Ashby, Jr., National Advisory Committee for Aeronautics, Washington, D.C. (Research memorandum L54I13), December1954
The collection consists of reports and papers on the subjects of pumps, turbines, fans, metering and flow (hydraulics).
Experimental investigation of an axial-flow compressor inlet stage operating at transonic relative inlet mach numbers, III - Blade-row performance of stage with transonic rotor and subsonic stator at corrected tip speeds of 800 and 1000 feet per second,
by Francis C. Schwenk, Seymour Lieblein and George W. Lewis, Jr., National Advisory Committee for Aeronautics, Washington, D.C. (Research memorandum E53G17), September1953
The collection consists of reports and papers on the subjects of pumps, turbines, fans, metering and flow (hydraulics).
Method of analysis for compressible flow through mixed-flow centrifugal impellers or arbitrary design,
by Joseph T. Hamrick, Ambrose Ginsburg and Walter M. Osborn, National Advisory Committee for Aeronautics (Technical note 2165), August1950
The collection consists of reports and papers on the subjects of pumps, turbines, fans, metering and flow (hydraulics).
Theoretical turbojet thrust augmentation by evaporation of water during compression as determined by use of a Mollier diagram,
by Arthur M. Trout, National Advisory Committee for Aeronautics, Washington, D.C., (Technical note 2104), June 1950
The collection consists of reports and papers on the subjects of pumps, turbines, fans, metering and flow (hydraulics).
Theoretical effect of inlet hub-tip-radius ratio and design specific mass flow on design performance of axial-flow compressors,
by Chung-Hua Wu, John T. Sinnette, Jr., and Robert E. Forrette, National Advisory Committee for Aeronautics, Washington, D.C. (Technical note 2068), April 1950
The collection consists of reports and papers on the subjects of pumps, turbines, fans, metering and flow (hydraulics).
An analysis of flow in rotating passage of large radial-inlet centrifugal compressor at tip speed of 700 feet per second,
by Vasily D. Prian and Donald J. Michel, National Advisory Committee for Aeronautics, Washington, D.C. (Technical note 2584), December1951
The collection consists of reports and papers on the subjects of pumps, turbines, fans, metering and flow (hydraulics).