Effects of leading-edge devices on the low-speed aerodynamic characteristics of a highly-swept arrow-wing
By: Samuel J. Scott, Oran W. Nicks, and P. K. Imbrie.
Contributors: Nicks, Oran W.; Imbrie, P. K.; Langley Research Center.
Series: NASA contractor report -- 172531.; NASA contractor report -- NASA CR-172531.
Publisher: National Aeronautics and Space Administration, Langley Research Center
Published: 1985
Place of publication: Hampton, Va
Language: eng
Format: Microform
Subjects: Leading edges (Aerodynamics); Airplanes -- Wings, Swept-back.; Leading edge slats.; Low speed.; Supersonic transports.; Swept wings.; Wind tunnel tests.
Notes: Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1985. 1 microfiche.