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Effect of nozzle inlet shape, lip thickness, and exit shape and size on subsonic jet noise

Effect of nozzle inlet shape, lip thickness, and exit shape and size on subsonic jet noise - - Washington, D.C. National Aeronautics & Space Administration 1973 - 19 p. - NASA TM X 68182 : 1977 .

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Universal Decimal Class. No.: LNASA TM X 68182 : 1977

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