Add to ORKGFuel consumption and weight analysis for vertical takeoff aircraft propulsion characteristic
Electric propulsion enables radical new vehicle concepts, particularly for Vertical Takeoff and Land...
NASA-Lewis sponsored two studies to determine the most promising convertible engine concepts for hig...
This study had the objectives of determining the most promising conventional and variable cycle engi...
Copyright @ 2010 The Royal Aeronautical Society. This article is the final author version of the pub...
Progress in vertical and short takeoff and landing (V/STOL) aircraft technology, in particular, duri...
In anticipation of an eventual VTOL requirement for civil aviation, NASA has been conducting studies...
The requirements for satisfactory characteristics in several key technology areas are discussed and ...
The gas turbine propulsion system has been playing the most significant role in the evolution and de...
A simplified mission analysis was performed to determine an optimum engine cycle for a 100-passenger...
The major challenges confronting the propulsion community for supersonic transport applications are ...
Turboshaft engine performance and weight models were developed to support conceptual propulsion and ...
This paper highlights the efforts being performed or sponsored by NASA, in cooperation with the U.S....
Technology associated with advanced conventional takeoff and landing transport aircraft is discussed...
The purpose of this paper is to give an outline of the present state of development and point out th...
The advancement of aeropropulsion systems continues to provide technology to various portions of the...
Electric propulsion enables radical new vehicle concepts, particularly for Vertical Takeoff and Land...
NASA-Lewis sponsored two studies to determine the most promising convertible engine concepts for hig...
This study had the objectives of determining the most promising conventional and variable cycle engi...
Copyright @ 2010 The Royal Aeronautical Society. This article is the final author version of the pub...
Progress in vertical and short takeoff and landing (V/STOL) aircraft technology, in particular, duri...
In anticipation of an eventual VTOL requirement for civil aviation, NASA has been conducting studies...
The requirements for satisfactory characteristics in several key technology areas are discussed and ...
The gas turbine propulsion system has been playing the most significant role in the evolution and de...
A simplified mission analysis was performed to determine an optimum engine cycle for a 100-passenger...
The major challenges confronting the propulsion community for supersonic transport applications are ...
Turboshaft engine performance and weight models were developed to support conceptual propulsion and ...
This paper highlights the efforts being performed or sponsored by NASA, in cooperation with the U.S....
Technology associated with advanced conventional takeoff and landing transport aircraft is discussed...
The purpose of this paper is to give an outline of the present state of development and point out th...
The advancement of aeropropulsion systems continues to provide technology to various portions of the...
Electric propulsion enables radical new vehicle concepts, particularly for Vertical Takeoff and Land...
NASA-Lewis sponsored two studies to determine the most promising convertible engine concepts for hig...
This study had the objectives of determining the most promising conventional and variable cycle engi...