Measuring and testing – Wind tunnel: aerodynamic wing and propeller study
Patent
1974-11-06
1976-10-05
Woodiel, Donald O.
Measuring and testing
Wind tunnel: aerodynamic wing and propeller study
G01M 900
Patent
active
039837491
ABSTRACT:
An annular arc accelerator shock tube employs a cold gas driver to flow a stream of gas from an expansion section through a high voltage electrode section to a test section, thus driving a shock wave in front of it. A glow discharge detects the shock wave and actuates a trigger generator which in turn fires spark-gap switches to discharge a bank of capacitors across a centered cathode and an annular anode in tandem electrode sections as the initial shock wave passes through the anode section from the cathode section thereby depositing energy into the flow gas without the necessity of any diaphragm opening in the gas flow from the expansion section through the electrode sections.
REFERENCES:
"Development of an Annular Arc Accelerator Shock Tube Driver", Leibowitz, July 1973, pp. 679-689, of Proceedings of the Ninth International Shock Tube Symposium, Stanford University.
Fletcher James C. Administrator of the National Aeronautics and Space
Leibowitz Lewis P.
Grifka Wilfred
Manning John R.
Mott Monte F.
Woodiel Donald O.
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