Orifice mass flow calculation in NASA's W-8 single stage axial compressor facility /

Bibliographic Details

Main Author:	Bozak, Richard F. (Author)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, February 2018.
Series:	NASA technical memorandum ; 2018-219762.
Subjects:	Mass flow. Orifice flow. Turbocompressors. Discharge coefficient. Static pressure.
Online Access:	https://purl.fdlp.gov/GPO/gpo89357