Aerodynamic design of the contoured wind-tunnel liner for the NASA supercritical, laminar-flow-control, swept-wing experiment
By: Perry A. Newman, E. Clay Anderson, and John B. Peterson, Jr
Contributors: Anderson, E. Clay; Peterson, John B; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Series: NASA technical paper -- 2335
Publisher: National Information Branch; For sale by the National Technical Information Service]
Published: 1984
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 41
Subjects: Aerodynamics, Transonic; Wind tunnels; Winged spacecraft -- Testing
Notes: Distributed to depository libraries in microfiche

"September 1984"--Cover

Subject category 02

Includes bibliographical references