Hot gas ingestion test results of a two-poster vectored thrust concept with flow visualization in the NASA Lewis 9- x 15-foot low speed wind tunnel

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Hot gas ingestion test results of a two-poster vectored thrust concept with flow visualization in the NASA Lewis 9- x 15-foot low speed wind tunnel

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First published: 1990

Subjects

Control systems design. Exhaust nozzles. Flow distribution. Flow visualization. High temperature gases. Inlet flow. Laser applications. Nozzle flow. Support systems. Thrust vector control.

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