Add to ORKGAccurately estimating turbine cooling requirements at a preliminary design stage is both a challenge...
An analysis of air refrigeration systems indicated that air cycles are generally less satisfactory t...
Increased attention to fuel economy and increased thrust requirements have increased the demand for ...
Turbine aerodynamic and cooling requirements for turbojet powered Mach 3 transport using methane fue
Effects of air-cooling turbine rotor blades on performance of a turbojet engine were calculated for ...
Because of financial and political constraints, strategic aerospace materials required for the hot s...
The effects of turbine-blade cooling on engine performance were analytically investigated for a turb...
Transpiration and convective cooling concepts are examined for the fuselage and tail surface of a Ma...
The analytical study presented examines the effects of varying turbine cooling assumptions on the pe...
Cascade investigation of cooling characteristics of air-cooled turbine blade for use in turboprop en...
An analysis has been made of the characteristics of several cooling cycles suitable for cockpit cool...
The thermal design of the combustor and turbine of a gas turbine engine poses a number of difficult ...
One of the significant ways in which the performance level of aircraft turbine engines has been impr...
A study was conducted to determine the effect of chord size on air cooled turbine blades. In the pre...
The system eliminates the necessity of shielding an aircraft airframe constructed of material such a...
Accurately estimating turbine cooling requirements at a preliminary design stage is both a challenge...
An analysis of air refrigeration systems indicated that air cycles are generally less satisfactory t...
Increased attention to fuel economy and increased thrust requirements have increased the demand for ...
Turbine aerodynamic and cooling requirements for turbojet powered Mach 3 transport using methane fue
Effects of air-cooling turbine rotor blades on performance of a turbojet engine were calculated for ...
Because of financial and political constraints, strategic aerospace materials required for the hot s...
The effects of turbine-blade cooling on engine performance were analytically investigated for a turb...
Transpiration and convective cooling concepts are examined for the fuselage and tail surface of a Ma...
The analytical study presented examines the effects of varying turbine cooling assumptions on the pe...
Cascade investigation of cooling characteristics of air-cooled turbine blade for use in turboprop en...
An analysis has been made of the characteristics of several cooling cycles suitable for cockpit cool...
The thermal design of the combustor and turbine of a gas turbine engine poses a number of difficult ...
One of the significant ways in which the performance level of aircraft turbine engines has been impr...
A study was conducted to determine the effect of chord size on air cooled turbine blades. In the pre...
The system eliminates the necessity of shielding an aircraft airframe constructed of material such a...
Accurately estimating turbine cooling requirements at a preliminary design stage is both a challenge...
An analysis of air refrigeration systems indicated that air cycles are generally less satisfactory t...
Increased attention to fuel economy and increased thrust requirements have increased the demand for ...