Add to ORKGTurbine aerodynamic and cooling requirements for turbojet powered Mach 3 transport using methane fue
The aerodynamic performance of a redesigned compressor drive turbine of the gas turbine engine is de...
The design of a single stage axial-flow turbine with a tip diameter of 11.15 cm is presented. The de...
Cold air study of high temperature gas turbine - blade feature effects on stator performanc
Approximate average midspan metal temperatures and coolant flow requirements for turbine airfoils co...
Afterburning turbojet, nonafterburning turbojet, and duct burning turbofan designs for supersonic tr...
Cascade investigation of cooling characteristics of air-cooled turbine blade for use in turboprop en...
Effects of air-cooling turbine rotor blades on performance of a turbojet engine were calculated for ...
The effects of turbine-blade cooling on engine performance were analytically investigated for a turb...
A study was made of an advanced technology airplane using supercritical aerodynamics. Cruise Mach nu...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1995.In...
DVL experimental and analytical work on the cooling of turbine blades by using ram air as the workin...
Computer program to generate turbine aerodynamic requirements, approximate external blade geometries...
The analytical study presented examines the effects of varying turbine cooling assumptions on the pe...
Performance characteristics and efficiency determined for air cooled turbojet engine suitable for su...
Methane or hydrogen fuel direct cooling of first stage stator of SST aircraft turbine - numerical he...
The aerodynamic performance of a redesigned compressor drive turbine of the gas turbine engine is de...
The design of a single stage axial-flow turbine with a tip diameter of 11.15 cm is presented. The de...
Cold air study of high temperature gas turbine - blade feature effects on stator performanc
Approximate average midspan metal temperatures and coolant flow requirements for turbine airfoils co...
Afterburning turbojet, nonafterburning turbojet, and duct burning turbofan designs for supersonic tr...
Cascade investigation of cooling characteristics of air-cooled turbine blade for use in turboprop en...
Effects of air-cooling turbine rotor blades on performance of a turbojet engine were calculated for ...
The effects of turbine-blade cooling on engine performance were analytically investigated for a turb...
A study was made of an advanced technology airplane using supercritical aerodynamics. Cruise Mach nu...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1995.In...
DVL experimental and analytical work on the cooling of turbine blades by using ram air as the workin...
Computer program to generate turbine aerodynamic requirements, approximate external blade geometries...
The analytical study presented examines the effects of varying turbine cooling assumptions on the pe...
Performance characteristics and efficiency determined for air cooled turbojet engine suitable for su...
Methane or hydrogen fuel direct cooling of first stage stator of SST aircraft turbine - numerical he...
The aerodynamic performance of a redesigned compressor drive turbine of the gas turbine engine is de...
The design of a single stage axial-flow turbine with a tip diameter of 11.15 cm is presented. The de...
Cold air study of high temperature gas turbine - blade feature effects on stator performanc