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