Add to ORKGThe state of the art of ejector technology is assessed and the desired direction of future studies in all aspects of ejector thrust augmenting systems is deliniated
The application and use of inlets and nozzles in aerospace, V/STOL, and hypersonic propulsion system...
A general parametric description is suggested for thrust augmentor application to STOL and V/STOL ai...
Unsteady ejectors are currently under investigation for use in some pulse detonation engine (PDE) pr...
A technique is developed for determining a representative value of the maximum efficiency that can b...
The conference on Turbojet-Engine Thrust-Augmentation Research was organized by the NACA to present ...
A study was directed towards assessing viability and effectiveness of an air augmented ejector/rocke...
The flow-field within a two-dimensional thrust augmenting ejector has been documented experimentally...
The present work was initiated due to the need for a method to understand and predict the thrust aug...
A large-scale, ejector-lift V/STOL Model, powered by a J-97 engine, was tested at the NASA Ames Rese...
Requirements were established for a conceptual design study to analyze and design an engine flow div...
A fundamental exploratory experiment is conducted assessing the performance of a one-sided ejector w...
With the emergence of V/STOL vehicles and unmanned aircrafts has come the resurgence of thrust augme...
A theoretical investigation of tail-pipe burning, water injection at the compressor inlet, combinati...
Procedures for matching intake and ejector pumping characteristics of air-augmented nozzle
Experimental studies were conducted to investigate the flow and the performance of thrust augmenting...
The application and use of inlets and nozzles in aerospace, V/STOL, and hypersonic propulsion system...
A general parametric description is suggested for thrust augmentor application to STOL and V/STOL ai...
Unsteady ejectors are currently under investigation for use in some pulse detonation engine (PDE) pr...
A technique is developed for determining a representative value of the maximum efficiency that can b...
The conference on Turbojet-Engine Thrust-Augmentation Research was organized by the NACA to present ...
A study was directed towards assessing viability and effectiveness of an air augmented ejector/rocke...
The flow-field within a two-dimensional thrust augmenting ejector has been documented experimentally...
The present work was initiated due to the need for a method to understand and predict the thrust aug...
A large-scale, ejector-lift V/STOL Model, powered by a J-97 engine, was tested at the NASA Ames Rese...
Requirements were established for a conceptual design study to analyze and design an engine flow div...
A fundamental exploratory experiment is conducted assessing the performance of a one-sided ejector w...
With the emergence of V/STOL vehicles and unmanned aircrafts has come the resurgence of thrust augme...
A theoretical investigation of tail-pipe burning, water injection at the compressor inlet, combinati...
Procedures for matching intake and ejector pumping characteristics of air-augmented nozzle
Experimental studies were conducted to investigate the flow and the performance of thrust augmenting...
The application and use of inlets and nozzles in aerospace, V/STOL, and hypersonic propulsion system...
A general parametric description is suggested for thrust augmentor application to STOL and V/STOL ai...
Unsteady ejectors are currently under investigation for use in some pulse detonation engine (PDE) pr...