An airfoil flutter model suspension system to accommodate large static transonic airloads /

Bibliographic Details

Main Author:	Reed, Wilmer H.
Corporate Authors:	DEI-Tech, Inc, Langley Research Center
Format:	Government Document eBook
Language:	English
Published:	Newport News, VA : Hampton, Va. : DEI-Tech, Inc. ; National Aeronautics and Space Administration, Langley Research Center, [1985]
Series:	NASA contractor report ; NASA CR-177998. NASA-CR-177998.
Subjects:	Airfoils. Blowdown wind tunnels. Flutter analysis. Pressure distribution. Static pressure. Supercritical airfoils. Transonic wind tunnels. Two dimensional flow.
Online Access:	https://purl.fdlp.gov/GPO/gpo21276