Measuring and testing – Wind tunnel: aerodynamic wing and propeller study
Patent
1997-02-27
1998-05-26
Dombroske, George M.
Measuring and testing
Wind tunnel: aerodynamic wing and propeller study
738656, 73756, G01M 906
Patent
active
057568928
ABSTRACT:
The invention as disclosed herein teaches apparatus whereby the instantaneous dynamic static pressure and the steady-state static pressure may be simultaneously measured within a supersonic or subsonic gaseous fluid flow field. The dynamic static pressure is measured by an electronic transducer and the steady-state static pressure is measured by pneumatic means.
REFERENCES:
patent: 2315756 (1943-04-01), Warner
patent: 3585859 (1971-06-01), DeLeo et al.
patent: 3677079 (1972-07-01), Hoeflinger
patent: 4703661 (1987-11-01), Evers
patent: 4783994 (1988-11-01), Ashby, Jr.
Ernst Michael A.
Porro A. Robert
Dombroske George M.
Felber Joseph L.
Stone Kent N.
The United States of America as represented by the United States
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