Accession Number : AD0775066
Title : Comments on NASA Langley Research on Transonic Unsteady Aerodynamics,
Corporate Author : ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT PARIS (FRANCE)
Personal Author(s) : Bland,Samuel R.
Report Date : DEC 1973
Pagination or Media Count : 14
Abstract : Research is reported in an effort to fill the need for accurate unsteady transonic aerodynamics for use in flutter calculation. The paper describes five different approaches to the transonic unsteady flow problem. These methods each attempt to take into account the nonconstant Mach number characteristic of transonic flow, some more accurately than others. Viscous effects are not included.
Descriptors : *Transonic flow, *Flutter, Nonlinear systems, Mach number, Aircraft, Stability
Subject Categories : Aerodynamics
Distribution Statement : APPROVED FOR PUBLIC RELEASE