The research objects of this study are new principles of gas turbine and rocket engines working process organization, based on the oscillatory motion of shock and detonation waves. Purpose is to identify the state of level technology, describe the subject area, state the direction of research and formulate the main problems hindering the implementation of wave technology into mass production. The results presented in the study can be recommended for developers of aircraft engines, power and technological turbo-machinery
This Thesis- ERAU Login Required is brought to you for free and open access by ERAU Scholarly Common...
Thesis (Sc. D.)--Massachusetts Institute of Technology, Dept. of Physics, 1938.Includes bibliographi...
Pulse detonation engines (PDEs) are new exciting propulsion technologies for future propulsion appli...
Detonation wave engines, thanks to their more efficient thermodynamic properties, are expected to ex...
The paper describes the distinctive features of the altitude-velocity characteristics of detonation ...
The subject of research in the article is engines operating on the detonation principle of convertin...
Using detonation rather than deflagration for a combustion mode in an engine could provide an increa...
Abstract:- Recent renewed interest in initiating detonation as a favorable combustion process prompt...
The paper contains analysis of the problems preventing from wide use of pulse detonation engines (PD...
The ideal thermodynamic cycle of a detonation engine is substantiated and a method of computing the ...
For some decades, efforts have been made to exploit nonsteady combustion and gas dynamic phenomenon....
Pulse Detonation Engine has high thermal efficiency for utilizing detonation and is planned to vario...
Detonation in the internal-combustion engine is studied as a physical process. It is shown that deto...
The subject of this paper is the experimental study of detonation wave phenomenon as related to prop...
A study on innovative combustion system for future aeroengine core concepts is done in the frame of ...
This Thesis- ERAU Login Required is brought to you for free and open access by ERAU Scholarly Common...
Thesis (Sc. D.)--Massachusetts Institute of Technology, Dept. of Physics, 1938.Includes bibliographi...
Pulse detonation engines (PDEs) are new exciting propulsion technologies for future propulsion appli...
Detonation wave engines, thanks to their more efficient thermodynamic properties, are expected to ex...
The paper describes the distinctive features of the altitude-velocity characteristics of detonation ...
The subject of research in the article is engines operating on the detonation principle of convertin...
Using detonation rather than deflagration for a combustion mode in an engine could provide an increa...
Abstract:- Recent renewed interest in initiating detonation as a favorable combustion process prompt...
The paper contains analysis of the problems preventing from wide use of pulse detonation engines (PD...
The ideal thermodynamic cycle of a detonation engine is substantiated and a method of computing the ...
For some decades, efforts have been made to exploit nonsteady combustion and gas dynamic phenomenon....
Pulse Detonation Engine has high thermal efficiency for utilizing detonation and is planned to vario...
Detonation in the internal-combustion engine is studied as a physical process. It is shown that deto...
The subject of this paper is the experimental study of detonation wave phenomenon as related to prop...
A study on innovative combustion system for future aeroengine core concepts is done in the frame of ...
This Thesis- ERAU Login Required is brought to you for free and open access by ERAU Scholarly Common...
Thesis (Sc. D.)--Massachusetts Institute of Technology, Dept. of Physics, 1938.Includes bibliographi...
Pulse detonation engines (PDEs) are new exciting propulsion technologies for future propulsion appli...