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Data reduction functions for the Langley 14- by 22-foot subsonic tunnel /

Bibliographic Details
Main Authors: Boney, Andy D. (Author), Nishikawa, Hiroaki (Author)
Corporate Author: United States. National Aeronautics and Space Administration (sponsoring body.)
Format: Government Document eBook
Language:English
Published: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 2014.
Series:NASA technical memorandum ; 2014-218513.
Subjects:
Data reduction.
Subsonic wind tunnels.
Flowmeters.
Jet exhaust.
Wall pressure.
Loads (forces)
Online Access:https://purl.fdlp.gov/GPO/gpo54991
http://purl.fdlp.gov/GPO/gpo54991
Description
Item Description:Title from title screen (viewed Feb. 3, 2015).
"August 2014."
Physical Description:1 online resource (iii, 77 pages).
Bibliography:Includes bibliographical references (page 77).