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
      Aerodynamics

Distribution Statement : APPROVED FOR PUBLIC RELEASE