Open AccessV-Tail flutter analysis of wing-in-surface-effect (WISE) aircraft using a structural analysis software
Author(s) -
Muhammad Kusni,
A. Taufiqurrahman,
Leonardo Gunawan
Publication year - 2021
Publication title -
iop conference series. materials science and engineering
Language(s) - English
Resource type - Journals
eISSN - 1757-899X
pISSN - 1757-8981
DOI - 10.1088/1757-899x/1173/1/012060
Subject(s) - flutter , aeroelasticity , structural engineering , flight envelope , fuselage , knot (papermaking) , wing , aerodynamic force , aerodynamics , engineering , envelope (radar) , control theory (sociology) , aerospace engineering , computer science , radar , chemical engineering , control (management) , artificial intelligence
Flutter is a dynamic aeroelastic instability that may cause structural failure and limits flight envelope of an aircraft. A passenger aircraft is required to be free from flutter and other aeroelastic instability phenomena, as stated in the regulations such as FAR 25. 33 / FAR 23.33. This paper presents the flutter analyses of the WISE aircraft using MSC Nastran. The analyses were carried out to the V-tail, one of the component where flutter might occur, by assuming rigid fuselage. Results of each analysis, in the form of velocity-damping and velocity-frequency curves, were evaluated to determine the critical flutter speed and frequency. First the analysis were conducted for sea level operation using KE, PK and PKNL methods which predict respectively the flutter speed of 1036 knot, 1037 knot, and 1037 knot. The three methods also consistently predict that the mode shapes involved in the flutter are the 5 th mode and the 3 rd mode. Then by using the PK-method, the analysis were repeated for air density variation. It is shown that the lower the air density, the higher the flutter speed is. It is concluded that tail flutter does not occur during the operation of the WISE craft with max operating speed of 80 knot.