Technical Memorandum 1 0 0 5 80 WING FLUTTER CALCULATIONS WITH THE CAP-TSD UNSTEADY TRANSONIC SMALL DISTURBANCE PROGRAM

The paper describes the application and assessment of the recently-developed CAP-TSD transonic small-disturbance code for flutter prediction. The CAP-TSD program has been developed for aeroelastic analysis of complete aircraft configurations and was previously applied lo the calculation of steady and unsteady pressures with favorable results. Flutter… CONTINUE READING