Modeling and control study of the NASA 0.3-meter transonic cryogenic tunnel for use with sulfur hexafluoride medium /

Bibliographic Details

Main Author:	Balakrishna, S.
Corporate Author:	Langley Research Center
Other Authors:	Kilgore, W. Allen
Format:	Government Document Book
Language:	English
Published:	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1992]
Series:	NASA contractor report ; NASA CR-189737.
Subjects:	Transonic wind tunnels. Sulfur hexafluoride. Aerodynamic characteristics. Cryogenic wind tunnels. Feedback control. Sulfur fluorides.
Online Access:	https://purl.fdlp.gov/GPO/LPS97272