Measuring and testing – Wind tunnel: aerodynamic wing and propeller study
Patent
1975-02-28
1976-01-06
Woodiel, Donald O.
Measuring and testing
Wind tunnel: aerodynamic wing and propeller study
G01M 900
Patent
active
039304108
ABSTRACT:
A solid missile body for testing in a wind tunnel with a solid body engine lume simulator having a passageway therethrough to simulate aspiration of the air mass at the juncture between the missile body and the engine plume.
REFERENCES:
patent: 3455155 (1969-07-01), Greenberg et al.
Edelberg Nathan
Gibson Robert P.
Murray Herbert H.
The United States of America as represented by the Secretary of
Woodiel Donald O.
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