Add to ORKGComputer program to generate turbine aerodynamic requirements, approximate external blade geometries, and coolant flow requirements for two stage axial flow turbin
The design of a single stage axial-flow turbine with a tip diameter of 11.15 cm is presented. The de...
Fortran 7094 computer program for calculation of design point performance of turbojet and turbofan e...
An air cooled version of a single-stage, axial-flow turbine was investigated to determine aerodynami...
The program method is based on a mean-diameter flow analysis. Input design requirements include powe...
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...
Several modifications have been made to the axial-flow turbine preliminary sizing code TURBAN. Turbi...
An algorithm is presented for calculating both the quantity of compressor bleed flow required to coo...
Two-stage, axial flow turbine test rig for providing cold flow aerodynamic performance data on Brayt...
Computer code TD2 computes design point velocity diagrams and performance for multistage, multishaft...
Cold air tests on axial flow turbine with transpiration cooled discrete hole stator blades to determ...
Turbine aerodynamic and cooling requirements for turbojet powered Mach 3 transport using methane fue
This technique is applicable to larger axial flow turbines which may or may not incorporate variable...
Analytical procedure and Fortran IV program for determining off-design performance of multistage axi...
Computer program calculates the velocity distribution and streamlines over widely separated blades o...
The design of a single stage axial-flow turbine with a tip diameter of 11.15 cm is presented. The de...
Fortran 7094 computer program for calculation of design point performance of turbojet and turbofan e...
An air cooled version of a single-stage, axial-flow turbine was investigated to determine aerodynami...
The program method is based on a mean-diameter flow analysis. Input design requirements include powe...
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...
Several modifications have been made to the axial-flow turbine preliminary sizing code TURBAN. Turbi...
An algorithm is presented for calculating both the quantity of compressor bleed flow required to coo...
Two-stage, axial flow turbine test rig for providing cold flow aerodynamic performance data on Brayt...
Computer code TD2 computes design point velocity diagrams and performance for multistage, multishaft...
Cold air tests on axial flow turbine with transpiration cooled discrete hole stator blades to determ...
Turbine aerodynamic and cooling requirements for turbojet powered Mach 3 transport using methane fue
This technique is applicable to larger axial flow turbines which may or may not incorporate variable...
Analytical procedure and Fortran IV program for determining off-design performance of multistage axi...
Computer program calculates the velocity distribution and streamlines over widely separated blades o...
The design of a single stage axial-flow turbine with a tip diameter of 11.15 cm is presented. The de...
Fortran 7094 computer program for calculation of design point performance of turbojet and turbofan e...
An air cooled version of a single-stage, axial-flow turbine was investigated to determine aerodynami...