Experimental investigation of aeroelastic deformation of slender wings at supersonic speeds using a video model deformation measurement technique /

Bibliographic Details

Main Author:	Erickson, Gary E. (Author)
Corporate Author:	United States. National Aeronautics and Space Administration (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, [2013]
Series:	NASA technical memorandum ; 217977.
Subjects:	Aerodynamic loads. Angle of attack. Dynamic pressure. Mach number. Static pressure. Trailing edge flaps. Optical measurement. Reynolds number.
Online Access:	https://purl.fdlp.gov/GPO/gpo40579 http://purl.fdlp.gov/GPO/gpo40579