Add to ORKGThe objectives and status of the propulsion portion of a program aimed at advancing the technology and establishing a data base appropriate for the possible future development of supersonic cruise aircraft are reviewed. Research related to exhaust nozzles, combustors, and inlets that is covered by the noise, pollution, and dynamics programs is described
Propulsion system characteristics for a long range, high subsonic (Mach 0.90 - 0.98), jet commercial...
The topics covered include the following: supersonic cruise, the High Speed Research (HSR) Program, ...
Research into hypersonic propulsion; i.e., supersonic combustion, was seriously initiated at the Lan...
The Supersonic Cruise Aircraft Resarch (SCAR) program identified significant improvements in the tec...
A broad overview of the scope of research presently being supported by NASA in aircraft propulsion i...
A second generation, economically viable, and environmentally acceptable supersonic aircraft is revi...
Sustained supersonic cruise propulsion systems for military applications are studied. The J79-5 in t...
A review of five NASA engine-oriented propulsion programs of major importance to civil aviation are ...
A study was conducted to determine the promising propulsion systems for advanced supersonic transpor...
NASA is responsible for advancing technologies related to air transportation. A sampling of the work...
Technical progress made in each of the disciplinary research areas affecting the design of supersoni...
NASA is conducting aeronautical research over a broad range of Mach numbers. In addition to the adva...
Reports on the following technologies are included: engine design, exhaust gases, use of composites,...
The results of an aircraft engine emission reduction study are reviewed in detail. The capability of...
The role of the Lewis Research Center in aeronautical propulsion is described. The state of the art ...
Propulsion system characteristics for a long range, high subsonic (Mach 0.90 - 0.98), jet commercial...
The topics covered include the following: supersonic cruise, the High Speed Research (HSR) Program, ...
Research into hypersonic propulsion; i.e., supersonic combustion, was seriously initiated at the Lan...
The Supersonic Cruise Aircraft Resarch (SCAR) program identified significant improvements in the tec...
A broad overview of the scope of research presently being supported by NASA in aircraft propulsion i...
A second generation, economically viable, and environmentally acceptable supersonic aircraft is revi...
Sustained supersonic cruise propulsion systems for military applications are studied. The J79-5 in t...
A review of five NASA engine-oriented propulsion programs of major importance to civil aviation are ...
A study was conducted to determine the promising propulsion systems for advanced supersonic transpor...
NASA is responsible for advancing technologies related to air transportation. A sampling of the work...
Technical progress made in each of the disciplinary research areas affecting the design of supersoni...
NASA is conducting aeronautical research over a broad range of Mach numbers. In addition to the adva...
Reports on the following technologies are included: engine design, exhaust gases, use of composites,...
The results of an aircraft engine emission reduction study are reviewed in detail. The capability of...
The role of the Lewis Research Center in aeronautical propulsion is described. The state of the art ...
Propulsion system characteristics for a long range, high subsonic (Mach 0.90 - 0.98), jet commercial...
The topics covered include the following: supersonic cruise, the High Speed Research (HSR) Program, ...
Research into hypersonic propulsion; i.e., supersonic combustion, was seriously initiated at the Lan...