Wave combustors for trans-atmospheric vehicles
The wave combustor is an air-breathing hypersonic propulsion system which utilizes shock and detonation waves to enhance fuel-air mixing and combustion in supersonic flow. An oblique shock wave in the combustor can act as a flameholder by increasing the pressure and temperature of the air-fuel mixtu...
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| Veröffentlicht in: | Journal of propulsion and power 1992-05, Vol.8 (3), p.709-713 |
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| container_title | Journal of propulsion and power |
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| creator | Menees, Gene P Adelman, Henry G Cambier, Jean-Luc Bowles, Jeffrey V |
| description | The wave combustor is an air-breathing hypersonic propulsion system which utilizes shock and detonation waves to enhance fuel-air mixing and combustion in supersonic flow. An oblique shock wave in the combustor can act as a flameholder by increasing the pressure and temperature of the air-fuel mixture and thereby decreasing the ignition delay. This engine, which is called the oblique detonation wave engine (ODWE), can then be utilized to provide a smaller, lighter vehicle or to provide a higher payload capability for a given vehicle weight. An analysis of the performance of a conceptual trans-atmospheric vehicle (TAV) powered by an ODWE is given here. |
| doi_str_mv | 10.2514/3.23536 |
| format | Article |
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| fulltext | fulltext |
| identifier | ISSN: 0748-4658 |
| ispartof | Journal of propulsion and power, 1992-05, Vol.8 (3), p.709-713 |
| issn | 0748-4658 1533-3876 |
| language | eng |
| recordid | cdi_nasa_ntrs_19920054354 |
| source | NASA Technical Reports Server; Alma/SFX Local Collection |
| subjects | combustion Combustion chambers shock waves Spacecraft Propulsion And Power supersonic flow |
| title | Wave combustors for trans-atmospheric vehicles |
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