Add to ORKGencouragement and continued interest throughout this work. The financia1 support from the Natura1 Sciences and Engineering Research Counci1 of Canada is acknowledged with thanks. i i The possibility of using an oblique detonation wave ramjet as a power plant for a hypersonic vehicle is examined. The performance of a model of a two dimensional oblique detonation wave ramjet is analyzed in terms of thrust, lift and fuel consumption
I focused my thesis on ramjet and their aim is to inform public with this type of drive, with histor...
Thesis (Ph. D.)--University of Washington, 1993The goal of this research is to develop a predictive ...
This thesis contains the results of a theoretical analysis of the performance of an inverted turboje...
Recently, supersonic combustion ramjets are more and more realised to become the next-generation ste...
Research was conducted into the alternatives to the supersonic combustion ramjet (scramjet) engine f...
Two conceptual designs of the oblique detonation wave ramjet are presented. The performance is evalu...
Hypersonic airbreathing propulsion is one of the top techniques for future aerospace flight, but the...
The aim of this paper is to present a mathematical model to predict the overall performance of an ob...
This work outlines the concept and design of a hypersonic combustor to study the stabilization of no...
A simulation model for the ramjet propulsion describing the strong coupling of thermodynamic and fli...
This study reports the first experiments of a large-scale hydrogen-fueled oblique detonation engine ...
Wave combustors, which include the Oblique Detonation Wave Engine (ODWE), are attractive propulsion ...
Detonation-based propulsion systems are desired due to their potential for thermodynamic cycle effic...
This article describes analytic solutions for hypersonic flow of a premixed reactive ideal gas over ...
Oblique detonation engines have significant potential as air-breathing propulsion units because they...
I focused my thesis on ramjet and their aim is to inform public with this type of drive, with histor...
Thesis (Ph. D.)--University of Washington, 1993The goal of this research is to develop a predictive ...
This thesis contains the results of a theoretical analysis of the performance of an inverted turboje...
Recently, supersonic combustion ramjets are more and more realised to become the next-generation ste...
Research was conducted into the alternatives to the supersonic combustion ramjet (scramjet) engine f...
Two conceptual designs of the oblique detonation wave ramjet are presented. The performance is evalu...
Hypersonic airbreathing propulsion is one of the top techniques for future aerospace flight, but the...
The aim of this paper is to present a mathematical model to predict the overall performance of an ob...
This work outlines the concept and design of a hypersonic combustor to study the stabilization of no...
A simulation model for the ramjet propulsion describing the strong coupling of thermodynamic and fli...
This study reports the first experiments of a large-scale hydrogen-fueled oblique detonation engine ...
Wave combustors, which include the Oblique Detonation Wave Engine (ODWE), are attractive propulsion ...
Detonation-based propulsion systems are desired due to their potential for thermodynamic cycle effic...
This article describes analytic solutions for hypersonic flow of a premixed reactive ideal gas over ...
Oblique detonation engines have significant potential as air-breathing propulsion units because they...
I focused my thesis on ramjet and their aim is to inform public with this type of drive, with histor...
Thesis (Ph. D.)--University of Washington, 1993The goal of this research is to develop a predictive ...
This thesis contains the results of a theoretical analysis of the performance of an inverted turboje...