Supersonic inlet test for a quiet supersonic transport technology demonstrator in the NASA Glenn 8-by 6-foot supersonic wind tunnel / Raymond Castner and Stephanie Simerly, Michael Rankin.

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Bibliographic Details
Online Access:	Online Access
Main Authors:	Castner, Raymond S. (Author), Simerly, Stephanie (Author), Rankin, Michael (Author)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, August 2018.
Series:	NASA technical memorandum ; 2018-219956.
Subjects:	Supersonic transports. Supersonic wind tunnels. Aerodynamic stability.

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Call Number:	NAS 1.15:2018-219956
NAS 1.15:2018-219956	Available