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

Bibliographic Details

Corporate Author:	NASA Glenn Research Center
Other Authors:	Lepicovsky, J.
Format:	Government Document Book
Language:	English
Published:	[Cleveland, Ohio] : Hanover, MD : National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for Aerospace Information ; [2002]
Series:	NASA technical memorandum ; 211894.
Subjects:	Transonic flutter. Unsteady aerodynamics. Rotary wings. Computerized simulation. Wind tunnels. Pressure measurement. Data integration.
Online Access:	https://purl.fdlp.gov/GPO/LPS42580