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
- Type
- text
- Format
- Electronic resourceLanguage material
- Language
- English
- 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 9, 2019.)
- 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>.