Wind tunnel model engine plume simulator with internal mass flow

Measuring and testing – Wind tunnel: aerodynamic wing and propeller study

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G01M 900

Patent

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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.

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