Wind tunnel results of the aerodynamic performance of a 1/8-scale model of a twin-engine transport with multi-element wing /

Bibliographic Details

Main Authors:	Laflin, Brenda E. Gile (Author), Applin, Zachary T. (Author), Jones, Kenneth M. (Author)
Format:	Government Document eBook
Language:	English
Published:	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 1997.
Series:	NASA technical memorandum ; 110304.
Subjects:	Angle of attack. Mach number. Pressure distribution. Reynolds number. Sideslip. Subsonic speed. Wings. Aerodynamic characteristics. Wind tunnel tests.
Online Access:	https://purl.fdlp.gov/GPO/gpo77851