The evolution and current status of selected recent variable cycle engine (VCE) studies are reviewed, and how the results were influenced by airplane requirements is described. Promising VCE concepts are described, their designs are simplified and the potential benefits in terms of aircraft performance are identified. This includes range, noise, emissions, and the time and effort it may require to ensure technical readiness of sufficient depth to satisfy reasonable economic, performance, and environmental constraints. A brief overview of closely related, ongoing technology programs in acoustics and exhaust emissions is also presented. Realistic technology advancements in critical areas combined with well matched aircraft and selected VCE co...
The need for greatly improved fuel efficiency and off-design subsonic characteristics is discussed. ...
A second generation, economically viable, and environmentally acceptable supersonic aircraft is revi...
The evaluation of components of an advanced propulsion system for a future supersonic cruise vehicle...
Progress and the current status of the Variable Cycle Engine (VCE) study are reviewed with emphasis ...
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 Variable Stream Control Engine is studied for advanced supersonic cruise aircraft. Significant e...
The product/study double bypass variable cycle engine (VCE) was updated to incorporate recent improv...
Three proposed SCAR propulsion systems in terms of aircraft range for a fixed payload and take-off g...
Sideline noise and takeoff field length were varied for two types of Mach 2.32 cruise airplane to de...
This study had the objectives of determining the most promising conventional and variable cycle engi...
The impact of advanced supersonic technologies on the performance and characteristics of a supersoni...
Variable cycle engines were identified, based on the mixed-flow low-bypass-ratio augmented turbofan ...
Sustained supersonic cruise propulsion systems for military applications are studied. The J79-5 in t...
The need for greatly improved fuel efficiency and off-design subsonic characteristics is discussed. ...
A second generation, economically viable, and environmentally acceptable supersonic aircraft is revi...
The evaluation of components of an advanced propulsion system for a future supersonic cruise vehicle...
Progress and the current status of the Variable Cycle Engine (VCE) study are reviewed with emphasis ...
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 Variable Stream Control Engine is studied for advanced supersonic cruise aircraft. Significant e...
The product/study double bypass variable cycle engine (VCE) was updated to incorporate recent improv...
Three proposed SCAR propulsion systems in terms of aircraft range for a fixed payload and take-off g...
Sideline noise and takeoff field length were varied for two types of Mach 2.32 cruise airplane to de...
This study had the objectives of determining the most promising conventional and variable cycle engi...
The impact of advanced supersonic technologies on the performance and characteristics of a supersoni...
Variable cycle engines were identified, based on the mixed-flow low-bypass-ratio augmented turbofan ...
Sustained supersonic cruise propulsion systems for military applications are studied. The J79-5 in t...
The need for greatly improved fuel efficiency and off-design subsonic characteristics is discussed. ...
A second generation, economically viable, and environmentally acceptable supersonic aircraft is revi...
The evaluation of components of an advanced propulsion system for a future supersonic cruise vehicle...