Several modifications have been made to the axial-flow turbine preliminary sizing code TURBAN. Turbine cooling has been added to the analysis. New alternative input options allow direct specification of stage reaction, stage work factor, and stage work split. The Reynolds number loss dependency was modified and an internal calculation of air viscosity was added. A complete description of input and output along with sample cases are included
An air cooled version of a single-stage, axial-flow turbine was investigated to determine aerodynami...
A cursory review is presented of some of the recent work that has been done in turbine aerodynamic r...
Modeling enhancements made to a radial-inflow turbine conceptual design code are documented in this ...
This mean diameter flow analysis uses a stage average velocity diagram as the basis for the computat...
Blading models added to TURBAN, an axial turbine meanline design code, and CSPAN, an axial compresso...
Computer code TD2 computes design point velocity diagrams and performance for multistage, multishaft...
Computer program to generate turbine aerodynamic requirements, approximate external blade geometries...
The program method is based on a mean-diameter flow analysis. Input design requirements include powe...
Modifications made to the axial-flow compressor conceptual design code CSPAN are documented in this ...
Efficiency, mass flow rate, torque, and exit diffuser effectiveness of 5-inch axial flow turbin
An algorithm is presented for calculating both the quantity of compressor bleed flow required to coo...
A single-stage axial-flow turbine was investigated to determine the effect of increased stator throa...
A numerical study of the unsteady aerodynamic and thermal environment associated with axial turbine ...
An axial-flow turbine off-design performance computer code used for preliminary studies of gas turbi...
The design of a single stage axial-flow turbine with a tip diameter of 11.15 cm is presented. The de...
An air cooled version of a single-stage, axial-flow turbine was investigated to determine aerodynami...
A cursory review is presented of some of the recent work that has been done in turbine aerodynamic r...
Modeling enhancements made to a radial-inflow turbine conceptual design code are documented in this ...
This mean diameter flow analysis uses a stage average velocity diagram as the basis for the computat...
Blading models added to TURBAN, an axial turbine meanline design code, and CSPAN, an axial compresso...
Computer code TD2 computes design point velocity diagrams and performance for multistage, multishaft...
Computer program to generate turbine aerodynamic requirements, approximate external blade geometries...
The program method is based on a mean-diameter flow analysis. Input design requirements include powe...
Modifications made to the axial-flow compressor conceptual design code CSPAN are documented in this ...
Efficiency, mass flow rate, torque, and exit diffuser effectiveness of 5-inch axial flow turbin
An algorithm is presented for calculating both the quantity of compressor bleed flow required to coo...
A single-stage axial-flow turbine was investigated to determine the effect of increased stator throa...
A numerical study of the unsteady aerodynamic and thermal environment associated with axial turbine ...
An axial-flow turbine off-design performance computer code used for preliminary studies of gas turbi...
The design of a single stage axial-flow turbine with a tip diameter of 11.15 cm is presented. The de...
An air cooled version of a single-stage, axial-flow turbine was investigated to determine aerodynami...
A cursory review is presented of some of the recent work that has been done in turbine aerodynamic r...
Modeling enhancements made to a radial-inflow turbine conceptual design code are documented in this ...
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