Add to ORKGPerformance of turbine driven V/STOL cruise fan propulsion system at subsonic Mach number
The overall and blade-element performance of a low pressure ratio, low tip speed fan stage is presen...
Engine performance and mission studies were carried out for turbofan engines equipped with supersoni...
A 16-inch-diameter supersonic impulse rotor with guide vsnes was designed and tested in Freon-X?. Th...
Performance of turbine driven V/STOL cruise fan propulsion system at subsonic Mach numbers.Includes ...
Wind tunnel tests of subsonic aerodynamic characteristics of large scale tip turbine cruise fan with...
Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 22).Mode of ac...
Theoretical analysis of performance of a ducted-fan power plant designed both for high-output, high-...
The author has written a concise summary of the com-putational/experimental techniques that are pres...
Meeting NASA's N+3 goals requires a fundamental shift in approach to aircraft and engine design...
An isolated 1.15 pressure ratio turbofan engine simulator was tested at Mach numbers from 0.6 to 0.8...
Partial admission performance was obtained for a 0.4 linear scale version of the LF460 lift fan turb...
A study was conducted to assess the performance potential of a supersonic through-flow fan engine fo...
Meeting NASA's N+3 goals requires a fundamental shift in approach to aircraft and engine design...
This paper presents an engine sizing and cycle selection study of ultra high bypass ratio engines ap...
Effects of variable turbine area on subsonic cruise performance of turbojets designed for supersonic...
The overall and blade-element performance of a low pressure ratio, low tip speed fan stage is presen...
Engine performance and mission studies were carried out for turbofan engines equipped with supersoni...
A 16-inch-diameter supersonic impulse rotor with guide vsnes was designed and tested in Freon-X?. Th...
Performance of turbine driven V/STOL cruise fan propulsion system at subsonic Mach numbers.Includes ...
Wind tunnel tests of subsonic aerodynamic characteristics of large scale tip turbine cruise fan with...
Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 22).Mode of ac...
Theoretical analysis of performance of a ducted-fan power plant designed both for high-output, high-...
The author has written a concise summary of the com-putational/experimental techniques that are pres...
Meeting NASA's N+3 goals requires a fundamental shift in approach to aircraft and engine design...
An isolated 1.15 pressure ratio turbofan engine simulator was tested at Mach numbers from 0.6 to 0.8...
Partial admission performance was obtained for a 0.4 linear scale version of the LF460 lift fan turb...
A study was conducted to assess the performance potential of a supersonic through-flow fan engine fo...
Meeting NASA's N+3 goals requires a fundamental shift in approach to aircraft and engine design...
This paper presents an engine sizing and cycle selection study of ultra high bypass ratio engines ap...
Effects of variable turbine area on subsonic cruise performance of turbojets designed for supersonic...
The overall and blade-element performance of a low pressure ratio, low tip speed fan stage is presen...
Engine performance and mission studies were carried out for turbofan engines equipped with supersoni...
A 16-inch-diameter supersonic impulse rotor with guide vsnes was designed and tested in Freon-X?. Th...