FIELD: experimental aerodynamics, solves the problem of improvement of the prechambers of aerodynamic tunnels with a pulse working cycle.
SUBSTANCE: the prechamber consists of a body, check valve, hypersonic nozzle and transducers. Besides, the prechamber is provided with obturation rings installed in the joints of the device components. The prechamber cavity is sphere-shaped.
EFFECT: enhanced reliability of the device.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| PULSE ALTITUDE TUBE | 2010 |
|
RU2439523C1 |
| WIND TUNNEL | 2010 |
|
RU2436058C1 |
| AERODYNAMIC TUBE | 2014 |
|
RU2578052C1 |
| AERODYNAMIC UNIT OF ADIABATIC COMPRESSION WITH TWO PRECHAMBERS | 1970 |
|
SU1840955A1 |
| ADIABETIC COMPRESSION AERODYNAMIC FACILITY | 1971 |
|
SU1840308A1 |
| HYPERSONIC SHOCK AERODYNAMIC PIPE | 2016 |
|
RU2621367C1 |
| PROCESS OF PRODUCTION OF HYPERSONIC FLOW | 1996 |
|
RU2101691C1 |
| PRECHAMBER OF PISTON AERODYNAMIC UNIT | 1967 |
|
SU1840952A1 |
| METHOD FOR GENERATION WORKING GAS IN IMPULSE TUNNEL | 2014 |
|
RU2567097C1 |
| PRECHAMBER OF PISTON WIND TUNNEL | 1969 |
|
SU1840954A1 |
Authors
Dates
2006-09-10—Published
1965-09-16—Filed