Add to ORKGThe gas turbine propulsion system has been playing the most significant role in the evolution and de...
High speed propulsion employing turbojets, turbofans and variable cycle engines is interpreted here ...
DVL experimental and analytical work on the cooling of turbine blades by using ram air as the workin...
This analysis investigates the application of gas turbine engines at a cruise Mach number of 4
An analytical investigation was made of two supersonic interceptor type airplanes to determine the m...
Performance prediction of methane-fueled supersonic transports over range of cruise speeds up to Mac...
The performance of hypothetical turbojet systems, without thrust augmentation, as power plants for s...
Effect of high altitude on performance & operating characteristics of turbojet engines with hydrogen...
Liquid methane, which can be manufactured from any of the hydrocarbon sources such as coal, shale bi...
Calculated design-point performance of ram-jet engines using JP-4 fuel is presented for a wide range...
For the past several decades, research dealing with hypersonic flight regimes has been restricted ma...
Combustion efficiency of gaseous hydrogen fuel for ramjets at very high altitudes and high distortio
A parametric study of an integrated airframe and engine is presented for a hypersonic transport at a...
The gas turbine propulsion system has been playing the most significant role in the evolution and de...
The gas turbine propulsion system has been playing the most significant role in the evolution and de...
The gas turbine propulsion system has been playing the most significant role in the evolution and de...
High speed propulsion employing turbojets, turbofans and variable cycle engines is interpreted here ...
DVL experimental and analytical work on the cooling of turbine blades by using ram air as the workin...
This analysis investigates the application of gas turbine engines at a cruise Mach number of 4
An analytical investigation was made of two supersonic interceptor type airplanes to determine the m...
Performance prediction of methane-fueled supersonic transports over range of cruise speeds up to Mac...
The performance of hypothetical turbojet systems, without thrust augmentation, as power plants for s...
Effect of high altitude on performance & operating characteristics of turbojet engines with hydrogen...
Liquid methane, which can be manufactured from any of the hydrocarbon sources such as coal, shale bi...
Calculated design-point performance of ram-jet engines using JP-4 fuel is presented for a wide range...
For the past several decades, research dealing with hypersonic flight regimes has been restricted ma...
Combustion efficiency of gaseous hydrogen fuel for ramjets at very high altitudes and high distortio
A parametric study of an integrated airframe and engine is presented for a hypersonic transport at a...
The gas turbine propulsion system has been playing the most significant role in the evolution and de...
The gas turbine propulsion system has been playing the most significant role in the evolution and de...
The gas turbine propulsion system has been playing the most significant role in the evolution and de...
High speed propulsion employing turbojets, turbofans and variable cycle engines is interpreted here ...
DVL experimental and analytical work on the cooling of turbine blades by using ram air as the workin...