Add to ORKGVarious design concepts for a variable cycle engine applicable to a supersonic, mixed mission propulsion system which would combine the merits of a turbofan at subsonic operating conditions with those of a turbojet for supersonic operating conditions are briefly examined. In particular the integration of the variable area bypass injector with the core driven (aft fan block) fan stage is discussed and the technical benefits of the configuration are summarized
This study had the objectives of determining the most promising conventional and variable cycle engi...
The performance of candidate supersonic cruise inlets is reviewed and the aerodynamic installation p...
The ability of a part span variable inlet guide vane (VIGV) to modulate the thrust of a high bypass ...
Variable cycle engines were identified, based on the mixed-flow low-bypass-ratio augmented turbofan ...
An evaluation of various advanced propulsion concepts for supersonic cruise aircraft resulted in the...
Progress and the current status of the Variable Cycle Engine (VCE) study are reviewed with emphasis ...
The evaluation of components of an advanced propulsion system for a future supersonic cruise vehicle...
Three propulsion systems for a Mach 2 STOVL fighter were compared. The three propulsion systems are:...
Engine performance and mission studies were carried out for a single-spool Turbine Bypass Engine con...
The Variable Stream Control Engine is studied for advanced supersonic cruise aircraft. Significant e...
Wind tunnel tests were conducted to evaluate the aerodynamic performance of a coannular exhaust nozz...
Engine performance and mission studies were carried out for turbofan engines equipped with supersoni...
The product/study double bypass variable cycle engine (VCE) was updated to incorporate recent improv...
The evolution and current status of selected recent variable cycle engine (VCE) studies are reviewed...
Engine performance and mission studies were performed for turbofan engines with supersonic through-f...
This study had the objectives of determining the most promising conventional and variable cycle engi...
The performance of candidate supersonic cruise inlets is reviewed and the aerodynamic installation p...
The ability of a part span variable inlet guide vane (VIGV) to modulate the thrust of a high bypass ...
Variable cycle engines were identified, based on the mixed-flow low-bypass-ratio augmented turbofan ...
An evaluation of various advanced propulsion concepts for supersonic cruise aircraft resulted in the...
Progress and the current status of the Variable Cycle Engine (VCE) study are reviewed with emphasis ...
The evaluation of components of an advanced propulsion system for a future supersonic cruise vehicle...
Three propulsion systems for a Mach 2 STOVL fighter were compared. The three propulsion systems are:...
Engine performance and mission studies were carried out for a single-spool Turbine Bypass Engine con...
The Variable Stream Control Engine is studied for advanced supersonic cruise aircraft. Significant e...
Wind tunnel tests were conducted to evaluate the aerodynamic performance of a coannular exhaust nozz...
Engine performance and mission studies were carried out for turbofan engines equipped with supersoni...
The product/study double bypass variable cycle engine (VCE) was updated to incorporate recent improv...
The evolution and current status of selected recent variable cycle engine (VCE) studies are reviewed...
Engine performance and mission studies were performed for turbofan engines with supersonic through-f...
This study had the objectives of determining the most promising conventional and variable cycle engi...
The performance of candidate supersonic cruise inlets is reviewed and the aerodynamic installation p...
The ability of a part span variable inlet guide vane (VIGV) to modulate the thrust of a high bypass ...