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Modifications to the Langley 8-foot transonic pressure tunnel for the laminar flow control experiment

Modifications to the Langley 8-foot transonic pressure tunnel for the laminar flow control experiment - - Washington, D.C. National Aeronautics and Space Admin 1988 - 121 p. - NASA TM 4032 : 1988 .

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Subjects--Topical Terms:

Laminar flow control, Wind tunnels

Universal Decimal Class. No.: LNASA TM 4032 : 1988

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