Measuring and testing – Wind tunnel: aerodynamic wing and propeller study
Patent
1989-01-25
1990-02-06
Woodiel, Donald O.
Measuring and testing
Wind tunnel: aerodynamic wing and propeller study
G01M 900
Patent
active
048980285
ABSTRACT:
A piston is provided which serves to produce a pressure surge in a wind tunnel. Under the action of a gas pressure of at least 20 bars the piston is propelled in a first passage from an initial position to a target surface. Under the compression produced by the approaching piston, a diaphragm disposed at the end of the first passage is torn. The resulting pressure surge is transmitted in a second passage, which is filled with a testing gas, to a thin sheet. That thin sheet is torn so that the testing gas can enter a testing chamber as a supersonic shock wave. The piston is provided at its rear end with a locking extension, which cooperates with a stationary holder when the piston is in its initial position.
REFERENCES:
patent: 3983749 (1976-10-01), Fletcher
patent: 4363237 (1982-12-01), Creel, Jr. et al.
Metallgesellschaft Aktiengesellschaft
Woodiel Donald O.
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