Aerodynamic characteristics of two NASA supercritical airfoils with different maximum thicknesses

Aerodynamic characteristics of two NASA supercritical airfoils with different maximum thicknesses

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Bibliographic Details
Author / Creator:Harris, Charles D., 1952- author.
Imprint:Washington, D.C. : National Aeronautics and Space Administration, April 1972.
Description:1 online resource (55 pages) : illustrations.
Language:English
Series:NASA technical memorandum ; NASA TM X-2532
NASA technical memorandum ; X-2532.
Subject:
Transonic wind tunnels.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/10783579
Hidden Bibliographic Details
Other authors / contributors:Langley Research Center.
United States. National Aeronautics and Space Administration, issuing body, sponsoring body.
Notes:Title from title screen (viewed on May 3, 2016).
"April 1972."
"Performing organization: NASA Langley Research Center, Hampton, Va."--Report documentation page.
Includes bibliographical references (page 10).
Sponsored by the National Aeronautics and Space Administration 742-73-01-14
L-8173
Other form:Microfiche version: Harris, Charles D., 1952- Aerodynamic characteristics of two NASA supercritical airfoils with different maximum thicknesses
GPO item no.:0830-D (online)
Govt.docs classification:NAS 1.15:2532

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