Aerodynamic design of the contoured wind-tunnel liner for the NASA supercritical, laminar-flow-control, swept-wing experiment /

Aerodynamic design of the contoured wind-tunnel liner for the NASA supercritical, laminar-flow-control, swept-wing experiment /

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Bibliographic Details
Main Author: Newman, Perry A
Corporate Author: United States National Aeronautics and Space Administration. Scientific and Technical Information Branch
Other Authors: Anderson, E. Clay, Peterson, John B
Format: Government Document Book
Language:English
Published: Washington, D.C. : [Springfield, Va. : National Information Branch ; For sale by the National Technical Information Service], 1984
Series:NASA technical paper ; 2335
Subjects:
Aerodynamics, Transonic
Wind tunnels
Winged spacecraft > Testing

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Duke University

Holdings details from Duke University
Call Number: NAS 1.60:2335

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