Effect of Reynolds number and Mach number on flow angularity probe sensitivity /

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Created Date
1986
Description

Prepared at Langley Research Center.

September 1986.

Includes bibliographical references (p. 4-5).

Creator
Smith, Leigh Ann
Partner
HathiTrust
Contributing Institution
University of Illinois
Publisher
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service
Subjects
Transonic wind tunnels
Reynolds number
Mach number
Type
text
Format
Electronic resource
Language material
Language
English
URL
http://catalog.hathitrust.org/Record/011427073
Rights
Public domain. Learn more at http://www.hathitrust.org/access_use
Chicago citation style
Smith, Leigh Ann. Effect of Reynolds number and Mach number on flow angularity probe sensitivity /. 1986. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011427073. (Accessed December 13, 2018.)
APA citation style
Smith, Leigh Ann, (1986) Effect of Reynolds number and Mach number on flow angularity probe sensitivity /. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011427073
MLA citation style
Smith, Leigh Ann. Retrieved from the Digital Public Library of America <http://catalog.hathitrust.org/Record/011427073>.
Note: These citations are programmatically generated and may be incomplete.