Add to ORKGThe objectives and status of the propulsion program, along with the results acquired in the various technology areas, are discussed. The instrumentation requirements for and experience with flight testing the propulsion systems at high supersonic cruise are reported. Propulsion system performance differences between wind tunnel and flight are given. The effects of high frequency flow fluctuations (transients) on the stability of the propulsion system are described, and shock position control is evaluated
A true gust velocity measuring system designed to alleviate complications resulting from airframe fl...
From 1967 to 1997, pioneering propulsion flight research activities have been conceived and conducte...
Integration of propulsion and flight control systems and their optimization offers significant perfo...
The YF-12 research program was initiated to establish a technology base for the design of an efficie...
The history of NASA's interest in supersonic research and the agency's contribution to the developme...
The response of terminal-shock position and static pressures in the subsonic duct of a YF-12 aircraf...
The propulsion control requirements of supersonic aircraft are presented. Integration of inlet, engi...
A computer simulation of the YF-12 aircraft motions and propulsion system dynamics is presented. The...
The objectives and status of the propulsion portion of a program aimed at advancing the technology a...
The handling qualities of the YF-12 airplane as observed during NASA research flights over the past ...
Papers presented by personnel from the Dryden Flight Research Center, the Lewis Research Center, and...
The overall scope of the NASA Lewis High Performance Aircraft Propulsion Research Program is present...
Digital integrated control systems are studied. Such systems allow minimization of undesirable inter...
Sustained supersonic cruise propulsion systems for military applications are studied. The J79-5 in t...
The Supersonics Project, part of NASA's Fundamental Aeronautics Program, contains a number of techni...
A true gust velocity measuring system designed to alleviate complications resulting from airframe fl...
From 1967 to 1997, pioneering propulsion flight research activities have been conceived and conducte...
Integration of propulsion and flight control systems and their optimization offers significant perfo...
The YF-12 research program was initiated to establish a technology base for the design of an efficie...
The history of NASA's interest in supersonic research and the agency's contribution to the developme...
The response of terminal-shock position and static pressures in the subsonic duct of a YF-12 aircraf...
The propulsion control requirements of supersonic aircraft are presented. Integration of inlet, engi...
A computer simulation of the YF-12 aircraft motions and propulsion system dynamics is presented. The...
The objectives and status of the propulsion portion of a program aimed at advancing the technology a...
The handling qualities of the YF-12 airplane as observed during NASA research flights over the past ...
Papers presented by personnel from the Dryden Flight Research Center, the Lewis Research Center, and...
The overall scope of the NASA Lewis High Performance Aircraft Propulsion Research Program is present...
Digital integrated control systems are studied. Such systems allow minimization of undesirable inter...
Sustained supersonic cruise propulsion systems for military applications are studied. The J79-5 in t...
The Supersonics Project, part of NASA's Fundamental Aeronautics Program, contains a number of techni...
A true gust velocity measuring system designed to alleviate complications resulting from airframe fl...
From 1967 to 1997, pioneering propulsion flight research activities have been conceived and conducte...
Integration of propulsion and flight control systems and their optimization offers significant perfo...