| タイトル | The Use of Steady and Unsteady Detonation Waves for Propulsion Systems |
| 著者（英） | Adelman, Henry G.; Cambier, Jean-Luc; Cavolowsky, John A.; Bowles, Jeffrey V.; Menees, Gene P. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1995-01-01 |
| 言語 | eng |
| 内容記述 | Detonation wave enhanced supersonic combustors such as the Oblique Detonation Wave Engine (ODWE) are attractive propulsion concepts for hypersonic flight. These engines utilize detonation waves to enhance fuel-air mixing and combustion. The benefits of wave combustion systems include shorter and lighter engines which require less cooling and generate lower internal drag. These features allow air-breathing operation at higher Mach numbers than the diffusive burning scramjet delaying the need for rocket engine augmentation. A comprehensive vehicle synthesis code has predicted the aerodynamic characteristics and structural size and weight of a typical single-stage-to-orbit vehicle using an ODWE. Other studies have focused on the use of unsteady or pulsed detonation waves. For low speed applications, pulsed detonation engines (PDE) have advantages in low weight and higher efficiency than turbojets. At hypersonic speeds, the pulsed detonations can be used in conjunction with a scramjet type engine to enhance mixing and provide thrust augmentation. |
| NASA分類 | Aircraft Propulsion and Power |
| 権利 | No Copyright |
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