Wind-tunnel investigation of effects of wing-leading-edge modifications on the high angle-of-attack characteristics of a T-tail low-wing general-aviation aircraft
By: E. Richard White ; prepared for Langley Research Center.
Contributors: Langley Research Center.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.; Kentron International.
Series: NASA contractor report -- 3636.; NASA contractor report -- NASA CR-3636.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1982
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 21
Subjects: Stalling (Aerodynamics); Spin (Aerodynamics); Leading edges (Aerodynamics)
Notes: "Kentron International, Inc."

"November 1982"--Cover.

Includes bibliographical references.

NAS1-1600.