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An Experimental Investigation of Thrust Vectoring Two-Dimensional Convergent-Divergent Nozzles Installed in a Twin-Engine Fighter Model at High Angles of Attack
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Type: BOOK - Published: 2018-07-17 - Publisher: Createspace Independent Publishing Platform

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An investigation was conducted in the Langley 16-Foot Transonic Tunnel to determine thrust vectoring capability of subscale 2-D convergent-divergent exhaust noz
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NASA Technical Paper
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