Heat-transfer characteristics of partially film coded plug nozzle on a J-85 afterburning turbojet engine (NASA technical memorandum, NASA TM X-3362)

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Heat-transfer characteristics of partially film coded plug nozzle on a J-85 afterburning turbojet engine (NASA technical memorandum , NASA TM X-3362) (ID: B0006W8Y5U)	Description and Photos \| More ads in Aircraft

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Heat-transfer characteristics of partially film coded plug nozzle on a J-85 afterburning turbojet engine (NASA technical memorandum , NASA TM X-3362)

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