Sweep effect on the drag of rows of perpendicular circular cylinders in a laminar boundary layer at supersonic free-stream velocities / by Milton Lamb and Robert L. Stallings, Jr.

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Bibliographic Details
Online Access:	Search for the full-text version of this title in HathiTrust
Main Author:	Lamb, Milton
Corporate Authors:	Langley Research Center, United States. National Aeronautics and Space Administration
Other Authors:	Stallings, Robert L.
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974.
Series:	NASA technical note ; D-7812.
Subjects:	Drag (Aerodynamics) Cylinders. Laminar flow. Boundary layer. Aerodynamics, Supersonic.

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Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.14:D-7812
NAS 1.14:D-7812	Available Place a Hold