Author:
Syamsuar Sayuti,Sampurno Budi,Mahasti Katia Mayang,Sakti Pratama Muchamad Bayu,Sasongko Triyono Widi,Kartika Nina,Suksmono Adityo,Aji Saputro Mohamad Ivan,Eskayudha Dimas Bahtera
Abstract
Abstract
Flutter is a rapid self-feeding motion which is caused by the interaction of aerodynamic, structural and inertial forces. Flutter can cause major damage on aircraft structure which can lead to fatal accident in aviation. Several methods have been evolved to avoid the flutter phenomena occur during the flight envelope of aircraft design. On this study, method was developed by Indonesian Aerospace which consist of Finite Element Method (FEM) analysis, Ground Vibration Test (GVT), and Wind Tunnel Flutter Test (WTT). Based on the study, FEM have similar results toward to Wind Tunnel Flutter Test conjunction the clean configuration of N219 aircraft half wing model.
Subject
General Physics and Astronomy
Reference18 articles.
1. Updating MSC/NASTRAN Models to Match Test Data;Ken;MSC 1991 World User’s Conference,1991
2. Aeroservoelastic Modeling and Validation of a ThrustVectoring F/A-18 Aircraft;Brenner,1996
3. Aircraft Aeroservoelastic Compensation Using Constrained Optimization;Cheng,1992
Cited by
1 articles.
订阅此论文施引文献
订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献