The Variable Stream Control Engine is studied for advanced supersonic cruise aircraft. Significant environmental and performance improvements relative to first generation supersonic turbojet engines are cited. Two separate flow streams, each with independent burner and nozzle systems are incorporated within the engine. By unique control of the exhaust temperatures and velocities in two coannular streams, significant reduction in jet noise is obtained
Engine performance and mission studies were carried out for a single-spool Turbine Bypass Engine con...
The performance of candidate supersonic cruise inlets is reviewed and the aerodynamic installation p...
A study was conducted to determine the promising propulsion systems for advanced supersonic transpor...
The variable stream control engine is determined to be the most promising propulsion system concept ...
A continuation of the NASA/P and WA study to evaluate various types of propulsion systems for advanc...
An evaluation of various advanced propulsion concepts for supersonic cruise aircraft resulted in the...
The evolution and current status of selected recent variable cycle engine (VCE) studies are reviewed...
The evaluation of components of an advanced propulsion system for a future supersonic cruise vehicle...
The need for greatly improved fuel efficiency and off-design subsonic characteristics is discussed. ...
Recent programs in the field of jet noise, sponsored by the NASA Lewis Research Center, have indicat...
This study had the objectives of determining the most promising conventional and variable cycle engi...
A new concept in aircraft propulsion is described in this work. In particular, variable jet engine i...
Sustained supersonic cruise propulsion systems for military applications are studied. The J79-5 in t...
Progress and the current status of the Variable Cycle Engine (VCE) study are reviewed with emphasis ...
The impact of advanced supersonic technologies on the performance and characteristics of a supersoni...
Engine performance and mission studies were carried out for a single-spool Turbine Bypass Engine con...
The performance of candidate supersonic cruise inlets is reviewed and the aerodynamic installation p...
A study was conducted to determine the promising propulsion systems for advanced supersonic transpor...
The variable stream control engine is determined to be the most promising propulsion system concept ...
A continuation of the NASA/P and WA study to evaluate various types of propulsion systems for advanc...
An evaluation of various advanced propulsion concepts for supersonic cruise aircraft resulted in the...
The evolution and current status of selected recent variable cycle engine (VCE) studies are reviewed...
The evaluation of components of an advanced propulsion system for a future supersonic cruise vehicle...
The need for greatly improved fuel efficiency and off-design subsonic characteristics is discussed. ...
Recent programs in the field of jet noise, sponsored by the NASA Lewis Research Center, have indicat...
This study had the objectives of determining the most promising conventional and variable cycle engi...
A new concept in aircraft propulsion is described in this work. In particular, variable jet engine i...
Sustained supersonic cruise propulsion systems for military applications are studied. The J79-5 in t...
Progress and the current status of the Variable Cycle Engine (VCE) study are reviewed with emphasis ...
The impact of advanced supersonic technologies on the performance and characteristics of a supersoni...
Engine performance and mission studies were carried out for a single-spool Turbine Bypass Engine con...
The performance of candidate supersonic cruise inlets is reviewed and the aerodynamic installation p...
A study was conducted to determine the promising propulsion systems for advanced supersonic transpor...