Status of linear boundary-layer stability theory and the en method, with emphasis on swept-wing applications
By: Jerry N. Hefner and Dennis M. Bushnell
Contributors: Bushnell, Dennis M; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office; Langley Research Center
Series: NASA technical paper -- 1645
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; For sale by the National Technical Information Service]
Published: 1980
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 47
Subjects: Laminar flow; Airplanes -- Wings, Swept-back; Boundary layer
Notes: "Langley Research Center."

"April 1980"--Cover

Subject Category 34

Includes bibliographical references