Methodology of blade unsteady pressure measurement in the NASA transonic flutter cascade /

Bibliographic Details

Main Author:	Lepicovsky, Jan (Author)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, October 2002.
Series:	NASA technical memorandum ; 2002-211894.
Subjects:	Transonic flutter. Unsteady aerodynamics. Rotary wings. Computerized simulation. Wind tunnels. Pressure measurement. Data integration.
Online Access:	https://purl.fdlp.gov/GPO/LPS42580