Search
CSV
RISDiscussion: “Flow Analyses in a Single-stage Propulsion Pump” (Lee, Y. T., Hah, C., and Loellbach, J., 1996, ASME J. Turbomach., 118, pp. 240–248)
Publisher: The American Society of Mechanical Engineers (ASME)
The Measurement of Boundary Layers on a Compressor Blade in Cascade: Part 3—Pressure Surface Boundary Layers and the Near Wake
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Using the facility described in Part 1 [23], 11 detailed velocity and turbulence intensity profiles are obtained on the pressure surface of a double circular arc compressor blade in cascade. ...
The Measurement of Boundary Layers on a Compressor Blade in Cascade: Part 2—Suction Surface Boundary Layers
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Using the facility described in Part 1 [29], eleven detailed velocity and turbulence intensity profiles are obtained on the suction surface of a double circular arc blade in cascade. At the ...
Discussion: “Prediction of Cascade Performance Using an Incompressible Navier–Stokes Technique” (Hobson, G. V., and Lakshminarayana, B., 1991, ASME J. Turbomach., 113, pp. 561–571)
Publisher: The American Society of Mechanical Engineers (ASME)
The Measurement of Boundary Layers on a Compressor Blade in Cascade: Part 1—A Unique Experimental Facility
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A unique cascade facility is described which permits the use of laser-Doppler velocimetry (LDV) to measure blade boundary layer profiles. Because of the need for a laser access window, the ...
The Measurement of Boundary Layers on a Compressor Blade in Cascade: Part 4—Flow Fields for Incidence Angles of −1.5 and −8.5 Degrees
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Measurements, made with laser Doppler velocimetry, about a double-circular-arc compressor blade in cascade are presented for −1.5 and −8.5 deg incidence angles and a chord Reynolds number near ...
Closure to “Discussion of ‘The Measurement of Boundary Layers on a Compressor Blade in Cascade: Part 4—Flow Fields for Incidence Angles of −1.5 and −8.5 Degrees’” (1990, ASME J. Turbomach., 112, p. 255)
Publisher: The American Society of Mechanical Engineers (ASME)
Measurement and Analysis of Total-Pressure Unsteadiness Data From an Axial-Flow Compressor Stage
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A fast-response, total-pressure probe was used with a periodically sampling and averaging data acquisition system to study the unsteady total-pressure field in an axial-flow turbomachine. Periodically ...
Measurements of the Tip Clearance Flow for a High-Reynolds-Number Axial-Flow Rotor
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A high-Reynolds-number pump (HIREP) facility has been used to acquire flow measurements in the rotor blade tip clearance region, with blade chord Reynolds numbers of 3,900,000 and 5,500,000. The ...
An Experimental Investigation of the Flow Through an Axial-Flow Pump
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The high Reynolds number pump (HIREP) facility at ARL Penn State has been used to perform a low-speed, large-scale experiment of the incompressible flow of water through a two-blade-row ...