FIELD: construction of adiabetic compression aerodynamic facility used in experimental aerodynamics.
SUBSTANCE: the facility has a bottle with gas, duct with a piston installed in it, prechamber with a nozzle and working member. A tube with a blind end and ports is positioned inside the bottle with gas. Besides, an auxiliary sealed spring-loaded piston with a check valve connecting the inner cavity of the piston with the inner cavity of the bottle is installed in the tube.
EFFECT: enhanced serviceability of the facility and safety of experiment.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ADIABETIC COMPRESSION AEROGASDYNAMIC FACILITY | 1967 |
|
SU1840310A1 |
| PULSE ALTITUDE TUBE | 2010 |
|
RU2439523C1 |
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|
RU2753982C1 |
| PISTON OF AERODYNAMIC FACILITY OF ADIABATIC COMPRESSION | 1969 |
|
SU1840309A1 |
| ADIABATIC COMPRESSION UNIT | 0 |
|
SU801702A1 |
| METHOD FOR ADIABATIC GAS COMPRESSION IN WIND TUNNEL | 0 |
|
SU1765741A1 |
| METHOD OF OBTAINING AIR FLOW AT FULL-SCALE PARAMETERS AND DEVICE FOR REALIZATION OF THIS METHOD | 1995 |
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| IMPULSE AERODYNAMIC PIPE WITH ELECTRIC ARC OR COMBINED HEATING OF WORKING GAS | 2016 |
|
RU2638087C1 |
| AERODYNAMIC UNIT OF ADIABATIC COMPRESSION WITH TWO PRECHAMBERS | 1970 |
|
SU1840955A1 |
