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:

MARC

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245 1 0 |a Sweep effect on the drag of rows of perpendicular circular cylinders in a laminar boundary layer at supersonic free-stream velocities /  |c by Milton Lamb and Robert L. Stallings, Jr. 
260 |a Washington, D.C. :  |b National Aeronautics and Space Administration ;  |a [Springfield, Va.] :  |b [For sale by the National Technical Information Service],  |c 1974. 
300 |a 16 pages :  |b illustrations ;  |c 27 cm. 
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490 1 |a NASA technical note ;  |v NASA TN D-7812. 
500 |a Cover title. 
500 |a Prepared at Langley Research Center. 
504 |a Includes bibliographical references (page 8) 
650 0 |a Drag (Aerodynamics)  |0 http://id.loc.gov/authorities/subjects/sh85039270. 
650 0 |a Cylinders.  |0 http://id.loc.gov/authorities/subjects/sh85035129. 
650 0 |a Laminar flow.  |0 http://id.loc.gov/authorities/subjects/sh85074205. 
650 0 |a Boundary layer.  |0 http://id.loc.gov/authorities/subjects/sh85016095. 
650 0 |a Aerodynamics, Supersonic.  |0 http://id.loc.gov/authorities/subjects/sh85001297. 
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