FIELD: engine engineering. SUBSTANCE: chamber consists of Laval nozzle and Hartmann resonator axially alined inside the housing. Between the inner side of the housing and outer side of the nozzle is a space. The space is a mixing chamber whose inlet portion is the throat that further goes into the diverging portion. EFFECT: improved design. 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| REACTION NOZZLE OF DETONATION COMBUSTION PULSATING ENGINE WITH CENTRAL BODY | 1993 |
|
RU2066779C1 |
| DETONATION COMBUSTION PULSATING ENGINE | 1993 |
|
RU2066778C1 |
| PULSEJET ENGINE DETONATION CHAMBER | 1993 |
|
RU2078969C1 |
| COMBINED CHAMBER OF DETONATION COMBUSTION PULSEJET ENGINE | 1993 |
|
RU2080466C1 |
| ADJUSTABLE DETONATION CHAMBER OF PULSEJET ENGINE | 1993 |
|
RU2078974C1 |
| INTERMITTENT DETONATION ENGINE | 2010 |
|
RU2435059C1 |
| METHOD AND DEVICE FOR PRODUCING THRUST | 2005 |
|
RU2296876C2 |
| INTERMITTENT DETONATION ENGINE | 2012 |
|
RU2490498C1 |
| DETONATION CHAMBER OF PULSE-JET ENGINE | 1994 |
|
RU2106509C1 |
| METHOD OF AIR JET ENGINE OPERATION WITH THRUST MODULES OF PULSATION-DETONATION COMBUSTION AND DEVICE TO THIS END | 2008 |
|
RU2375601C2 |
