Accession Number : AD0282002
Title : BASIC PRINCIPLES OF THE INDICIAL LIFTING-SURFACE FLUTTER-ANALYSIS PROCEDURE.
Descriptive Note : Final rept.,
Corporate Author : AEROJET-GENERAL CORP AZUSA CALIF
Personal Author(s) : Mazelsky ,Bernard ; Amey,Harry B. , Jr.
Report Date : MAY 1962
Pagination or Media Count : 38
Abstract : A method of flutter analysis utilizing indicial functions to represent the unsteady aerodynamics is described. Basic concepts are illustrated for a two-dimensional wing; the extension to a spanwise distorting wing is also discussed. Significant aerodynamic parameters pertinent to a highly swept, hypersonic delta wing are reviewed. For these wings the principal factor for adequate prediction of flutter is determination of the steady and quasi-steady aerodynamic influence coefficients. The unsteady contributions are shown to have a negligible effect on the flutter characteristics. (Author)
Descriptors : *FLUTTER, WINGS, TRIANGULAR WINGS, SWEPT WINGS, AERODYNAMICS, THEORY, MATHEMATICAL PREDICTION, HYPERSONIC VEHICLES, LIFT, ELASTIC PROPERTIES, DAMPING, HYPERSONICS, MATHEMATICAL ANALYSIS
Distribution Statement : APPROVED FOR PUBLIC RELEASE