Wind tunnel test of a risk-reduction wing/fuselage model to examine juncture-flow phenomena /

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, November 2016.
Series:	NASA technical memorandum ; 2016-219348.
Subjects:	Body-wing configurations. Flow distribution. Laser doppler velocimeters. Reynolds number. Subsonic wind tunnels. Wind tunnel models.
Online Access:	https://purl.fdlp.gov/GPO/gpo77510