Accession Number : ADP007807
Title : Transonic Aeroelastic Calculations in Both the Time and Frequency Domains,
Corporate Author : BRITISH AEROSPACE (MILITARY AIRCRAFT) LTD KINGSTON-UPON-THAMES (UNITED KINGDO M)
Personal Author(s) : Knott, M. J.
Report Date : MAR 1992
Pagination or Media Count : 8
Abstract : A method for exploring the flutter characteristics of wing-only configurations in the transonic flow regime is presented. At the heart of the method is the UTSP program, which solves the non-linear transonic small perturbation equation with or without the simultaneous integration of the structural equations of motion.
Descriptors : *FLUTTER, *TRANSONIC FLOW, CONFIGURATIONS, EQUATIONS, INTEGRATION, PERTURBATIONS, WINGS, GREAT BRITAIN.
Subject Categories : Fluid Mechanics
Distribution Statement : APPROVED FOR PUBLIC RELEASE