Amplified crossflow disturbances in the laminar boundary layer on swept wings with suction / J. Ray Dagenhart.

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Bibliographic Details
Online Access:	Search for the full-text version of this title in HathiTrust
Main Author:	Dagenhart, J. Ray
Corporate Authors:	United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Langley Research Center
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981.
Series:	NASA technical paper ; 1902.
Subjects:	Airplanes > Wings, Swept-back > Mathematical models. Laminar flow > Mathematical models. Boundary layer > Mathematical models.

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Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.60:1902
NAS 1.60:1902	Available Place a Hold