FIELD: experimental aerogasdynamics, applicable for aerogasdynamic investigations on adiabetic compression facilities.
SUBSTANCE: the facility has a bottle with gas, duct, prechamber with a nozzle and a working component. A piston and a mechanism of its fixation in the initial position are installed in the duct. Besides, the facility has a tube with a blind end and ports positioned in the cavity of the bottle with gas and joined to the end face of the facility duct. The mentioned ports are made on the tube section in the area of its joint to the mentioned duct.
EFFECT: enhanced serviceability of the facility and safety of experiment.
1 dwg
Title | Year | Author | Number |
---|---|---|---|
ADIABETIC COMPRESSION AERODYNAMIC FACILITY | 1971 |
|
SU1840308A1 |
METHOD FOR ADIABATIC GAS COMPRESSION IN WIND TUNNEL | 0 |
|
SU1765741A1 |
METHOD OF COMPRESSION OF GAS | 0 |
|
SU1665791A1 |
PISTON OF AERODYNAMIC FACILITY OF ADIABATIC COMPRESSION | 1969 |
|
SU1840309A1 |
METHOD OF OBTAINING AIR FLOW AT FULL-SCALE PARAMETERS AND DEVICE FOR REALIZATION OF THIS METHOD | 1995 |
|
RU2093716C1 |
PULSE ALTITUDE TUBE | 2010 |
|
RU2439523C1 |
METHOD OF ADIABATIC COMPRESSION OF GAS IN AERODYNAMIC INSTALLATION | 0 |
|
SU972931A1 |
METHOD OF CREATING FLOW IN WIND TUNNEL | 0 |
|
SU1496450A1 |
AERODYNAMIC TUBE | 2014 |
|
RU2578052C1 |
PISTON GAS-DYNAMIC INSTALLATION | 2020 |
|
RU2753982C1 |
Authors
Dates
2006-09-10—Published
1967-12-15—Filed