Amplified crossflow disturbances in the laminar boundary layer on swept wings with suction
By: J. Ray Dagenhart.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.; Langley Research Center.
Series: NASA technical paper -- 1902.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1981
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 87
Subjects: Airplanes -- Wings, Swept-back -- Mathematical models.; Laminar flow -- Mathematical models.; Boundary layer -- Mathematical models.
Notes: "Langley Research Center."

"November 1981"--Cover.

Subject Category 34.

Includes bibliographical references.