Add to ORKGDVL experimental and analytical work on the cooling of turbine blades by using ram air as the working fluid over a sector or sectors of the turbine annulus area is summarized. The subsonic performance of ram-jet, turbo-jet, and turbine-propeller engines with both constant pressure and pulsating-flow combustion is investigated. Comparison is made with the performance of a reciprocating engine and the advantages of the gas turbine and jet-propulsion engines are analyzed. Nacelle installation methods and power-level control are discussed
Experiments to determine the available increase in turbine horsepower achieved by increasing turbine...
Cold air study of high temperature gas turbine - blade feature effects on stator performanc
A single-stage axial-flow turbine was investigated to determine the effect of increased stator throa...
DVL experimental and analytical work on the cooling of turbine blades by using ram air as the workin...
The effects of turbine-blade cooling on engine performance were analytically investigated for a turb...
Small high-speed single-cylinder compression-ignition engines were tested to determine their perform...
Cascade investigation of cooling characteristics of air-cooled turbine blade for use in turboprop en...
An analytical and experimental investigation was made with a J33-A-9 engine to determine the effecti...
Effects of air-cooling turbine rotor blades on performance of a turbojet engine were calculated for ...
As a means of preparing for high-altitude flight with spark-ignition engines in conjunction with exh...
ABSTRACT Based on the experience gained with more than 80 machines operating worldwide in 50 and 60 ...
Gas turbine engines are extensively used in the aviation and power generation industries. They are u...
The fuel consumption of a modern compound engine with that of an advanced high pressure ratio turbof...
Propulsion system characteristics for a long range, high subsonic (Mach 0.90 - 0.98), jet commercial...
Experimental temperatures are presented for an air-cooled turbine rotor blade tested in an engine. T...
Experiments to determine the available increase in turbine horsepower achieved by increasing turbine...
Cold air study of high temperature gas turbine - blade feature effects on stator performanc
A single-stage axial-flow turbine was investigated to determine the effect of increased stator throa...
DVL experimental and analytical work on the cooling of turbine blades by using ram air as the workin...
The effects of turbine-blade cooling on engine performance were analytically investigated for a turb...
Small high-speed single-cylinder compression-ignition engines were tested to determine their perform...
Cascade investigation of cooling characteristics of air-cooled turbine blade for use in turboprop en...
An analytical and experimental investigation was made with a J33-A-9 engine to determine the effecti...
Effects of air-cooling turbine rotor blades on performance of a turbojet engine were calculated for ...
As a means of preparing for high-altitude flight with spark-ignition engines in conjunction with exh...
ABSTRACT Based on the experience gained with more than 80 machines operating worldwide in 50 and 60 ...
Gas turbine engines are extensively used in the aviation and power generation industries. They are u...
The fuel consumption of a modern compound engine with that of an advanced high pressure ratio turbof...
Propulsion system characteristics for a long range, high subsonic (Mach 0.90 - 0.98), jet commercial...
Experimental temperatures are presented for an air-cooled turbine rotor blade tested in an engine. T...
Experiments to determine the available increase in turbine horsepower achieved by increasing turbine...
Cold air study of high temperature gas turbine - blade feature effects on stator performanc
A single-stage axial-flow turbine was investigated to determine the effect of increased stator throa...