The program method is based on a mean-diameter flow analysis. Input design requirements include power or pressure ratio, flow, temperature, pressure, and speed. Turbine designs are generated for any specified number of stages and for any of three types of velocity diagrams (symmetrical, zero exit swirl, or impulse). Exit turning vanes can be included in the design. Program output includes inlet and exit annulus dimensions, exit temperature and pressure, total and static efficiencies, blading angles, and last-stage critical velocity ratios. The report presents the analysis method, a description of input and output with sample cases, and the program listing
Several modifications have been made to the axial-flow turbine preliminary sizing code TURBAN. Turbi...
The design of a single stage axial-flow turbine with a tip diameter of 11.15 cm is presented. The de...
An axial-flow turbine off-design performance computer code used for preliminary studies of gas turbi...
The program method is based on a mean-diameter flow analysis. Input design requirements include powe...
This mean diameter flow analysis uses a stage average velocity diagram as the basis for the computat...
Analytical procedure and Fortran IV program for determining off-design performance of multistage axi...
Computer program to generate turbine aerodynamic requirements, approximate external blade geometries...
Stream-filament analysis procedure and correlation of total pressure loss coefficients to form basis...
Computer program for design of axial flow turbines with velocity distribution gradients at stator an...
A computer program written in FORTRAN that may be used for the design analysis of radial-inflow turb...
This technique is applicable to larger axial flow turbines which may or may not incorporate variable...
This report summarizes some NASA Lewis (i.e., government owned) computer codes capable of being used...
Includes bibliographical references (pages 68-70)A user interactive computer program was developed f...
A brief description of the radial turbine and its analysis needs is followed by discussions of five ...
FORTRAN program for computerized design of axial flow pump by blade element analysi
Several modifications have been made to the axial-flow turbine preliminary sizing code TURBAN. Turbi...
The design of a single stage axial-flow turbine with a tip diameter of 11.15 cm is presented. The de...
An axial-flow turbine off-design performance computer code used for preliminary studies of gas turbi...
The program method is based on a mean-diameter flow analysis. Input design requirements include powe...
This mean diameter flow analysis uses a stage average velocity diagram as the basis for the computat...
Analytical procedure and Fortran IV program for determining off-design performance of multistage axi...
Computer program to generate turbine aerodynamic requirements, approximate external blade geometries...
Stream-filament analysis procedure and correlation of total pressure loss coefficients to form basis...
Computer program for design of axial flow turbines with velocity distribution gradients at stator an...
A computer program written in FORTRAN that may be used for the design analysis of radial-inflow turb...
This technique is applicable to larger axial flow turbines which may or may not incorporate variable...
This report summarizes some NASA Lewis (i.e., government owned) computer codes capable of being used...
Includes bibliographical references (pages 68-70)A user interactive computer program was developed f...
A brief description of the radial turbine and its analysis needs is followed by discussions of five ...
FORTRAN program for computerized design of axial flow pump by blade element analysi
Several modifications have been made to the axial-flow turbine preliminary sizing code TURBAN. Turbi...
The design of a single stage axial-flow turbine with a tip diameter of 11.15 cm is presented. The de...
An axial-flow turbine off-design performance computer code used for preliminary studies of gas turbi...