Numerical calculation of flutter of a diamond back wing

被引：0
|
作者：
Wu, Xiao-Sheng [1 ]
Wu, Jia-Sheng [1 ]
机构：
[1] School of Mechatronic Engineering, Beijing Institute of Technology, Beijing 100081, China
来源：
Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology | 2007年 / 27卷 / 05期
关键词：
Aerodynamics; -; Diamonds; Interfaces; (computer); Velocity;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
In order to study the flutter characteristics of diamond back wing, a first order code has been developed to interface a structural model with an unsteady Navier-Stokes fluid model. FLUENT 6.2 was chosen to calculate the unsteady aerodynamics. NASTRAN was chosen to analyse the structures. Initial testing of this code has been completed on AGARD 445.6 wings. Computational results agreed well with the experiments and the computed results of other researchers. The procedure is thus demonstrated to be accurate. The code was used to analyse the flutter characteristics of diamond back wing and obtained the flutter velocity and frequency of diamond back wing.
引用
收藏
页码：385 / 389
相关论文
共 50 条
  • [41] FLUTTER ANALYSIS OF A SUPERSONIC RING WING
    CRIMI, P
    ORDWAY, DE
    JOURNAL OF THE AEROSPACE SCIENCES, 1962, 29 (05): : 578 - 582
  • [42] Adaptive flutter suppression of an unswept wing
    Roy, ID
    Eversman, W
    JOURNAL OF AIRCRAFT, 1996, 33 (04): : 775 - 783
  • [43] NUMERICAL CALCULATION OF NONLINEAR AERODYNAMICS OF WING-BODY CONFIGURATIONS.
    Rusak, Z.
    Wasserstrom, E.
    Seginer, A.
    1600, (21):
  • [44] PARAMETRIC STUDY OF THE FLUTTER STABILITY OF A SWEPT-BACK HALF-WING WITH ENGINE NACELLE IN SUBSONIC FLOW
    FORSCHING, H
    KEISSLER, C
    ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN UND WELTRAUMFORSCHUNG, 1994, 18 (05): : 289 - 302
  • [45] About the Wing and Whirl Flutter of a Slender Wing-Propeller System
    Boehnisch, Nils
    Braun, Carsten
    Muscarello, Vincenzo
    Marzocca, Pier
    JOURNAL OF AIRCRAFT, 2024, 61 (04): : 1117 - 1130
  • [46] Faster but still accurate calculation of wing flutter using unsteady transonic Euler equations with approximate boundary conditions
    Zhu, Biao
    Qiao, Zhide
    Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University, 2009, 27 (03): : 289 - 293
  • [47] Numerical simulation of 3-D wing flutter with fully coupled fluid-structural interaction
    Chen, Xiangying
    Zha, Ge-Cheng
    Yang, Ming-Ta
    COMPUTERS & FLUIDS, 2007, 36 (05) : 856 - 867
  • [48] NUMERICAL CALCULATION OF THE THERMAL CONDUCTIVITY COEFFICIENT IN DIAMOND-COPPER COMPOSITE
    Boguszewski, Tomasz
    Ciupinski, Lukasz
    Kurzydlowski, Krzysztof J.
    COMPOSITES THEORY AND PRACTICE, 2008, 8 (03): : 232 - 235
  • [49] NUMERICAL CALCULATION OF SONIC FLOW AROUND AN AIRPLANE WING PROFILE BY INVERSE METHOD
    EUVRARD, D
    HUBERT, J
    RIGAUT, F
    TOURNEMI.G
    COMPTES RENDUS HEBDOMADAIRES DES SEANCES DE L ACADEMIE DES SCIENCES SERIE A, 1971, 273 (16): : 739 - &
  • [50] Numerical Analysis of Aerodynamic Characteristics of the HALE Diamond Joined-Wing Configuration UAV
    Junlei Sun
    Heping Wang
    Zhou Zhou
    Shan Lei
    JournalofHarbinInstituteofTechnology(NewSeries), 2019, 26 (06) : 31 - 45
12345