An experimental investigation of a wing-fuselage junction model in the NASA Langley 14- by 22-foot subsonic tunnel /

Bibliographic Details

Main Authors:	Kegerise, Michael A. (Author), Neuhart, Dan H. (Dan Howard), 1952- (Author)
Format:	Government Document eBook
Language:	English
Published:	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, June 2019.
Series:	NASA technical memorandum ; 2019-220286.
Subjects:	Computational fluid dynamics. Turbulence models. Infrared imagery. Subsonic wind tunnels. Flow distribution.
Online Access:	https://purl.fdlp.gov/GPO/gpo123541