Onset of condensation effects with an NACA 0012-64 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnel /

Bibliographic Details

Main Author:	Hall, Robert M. (Author)
Corporate Author:	Langley Research Center
Format:	Government Document eBook
Language:	English
Published:	[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Office, April 1979.
Series:	NASA technical paper ; 1385.
Subjects:	Airfoils. Cryogenic wind tunnels. Pressure distribution. Stagnation temperature. Supercooling.
Online Access:	https://purl.fdlp.gov/GPO/gpo70962