Measuring and testing – Wind tunnel: aerodynamic wing and propeller study
Patent
1994-09-13
1996-04-09
Chilcot, Richard
Measuring and testing
Wind tunnel: aerodynamic wing and propeller study
73 1207, G01L 2300
Patent
active
055050816
ABSTRACT:
A free piston shot tube tunnel having a high speed valve for releasing the piston to start the piston shot. A further feature of the present invention is a free piston shock tube/tunnel having a high speed valve for releasing pressure from the compression tube into the shock tube.
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Lacey, Jr. John J.
Lindahl Bruce C.
Aero Systems Engineering, Inc.
Biegel Ronald
Chilcot Richard
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