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

页码：385 / 389

共 50 条

[31] Numerical calculation of the drag force applied to particle pushing
Agaliotis, E.
Rosenberger, M. R.
Schvezov, C. E.
Ares, A. E.
JOURNAL OF CRYSTAL GROWTH, 2008, 310 (7-9) : 1366 - 1370
[32] Aeroelastic Analysis of Membrane Microair Vehicles-Part I: Flutter and Limit Cycle Analysis for Fixed-Wing Configurations
Attar, Peter J.
Gordnier, Raymond E.
Johnston, Jordan W.
Romberg, William A.
Parthasarathy, Ramkumar N.
JOURNAL OF VIBRATION AND ACOUSTICS-TRANSACTIONS OF THE ASME, 2011, 133 (02):
[33] Numerical calculation of wind loads over solar collectors
Mier-Torrecilla, M.
Herrera, E.
Doblare, M.
PROCEEDINGS OF THE SOLARPACES 2013 INTERNATIONAL CONFERENCE, 2014, 49 : 163 - 173
[34] Numerical Analysis of Bioinspired Tails in a Fixed-Wing Micro Air Vehicle
Barderas, Estela Barroso
Mora, Rafael Bardera
Rodriguez-Sevillano, Angel Antonio
Garcia, Juan Carlos Matias
AEROSPACE, 2023, 10 (09)
[35] NUMERICAL INVESTIGATION OF THE THREE-DIMENSIONAL FLOW STRUCTURE ABOUT A REVOLVING WING
Garmann, Daniel J.
Visbal, Miguel R.
Orkwis, Paul D.
PROCEEDINGS OF THE ASME FLUIDS ENGINEERING DIVISION SUMMER MEETING, 2012, VOL 1, PTS A AND B, SYMPOSIA, 2012, : 1581 - 1592
[36] Numerical simulation of a flapping four-wing micro-aerial vehicle
Tay, W. B.
van Oudheusden, B. W.
Bijl, H.
JOURNAL OF FLUIDS AND STRUCTURES, 2015, 55 : 237 - 261
[37] Numerical investigations on two-dimensional canard-wing aerodynamic interference
Lin, San-Yih
Chin, Yan-Shin
Wang, Yuh-Ying
1600, Publ by AIAA, Washington, DC, United States (31):
[38] Using the Numerical Simulation Analyzes the Influence of the Rear Wing on the Car's Aerodynamic
Guo, Huan-liang
Qin, Pin-pin
Cui, Rong-yao
2018 ASIA-PACIFIC CONFERENCE ON INTELLIGENT MEDICAL (APCIM) / 2018 7TH INTERNATIONAL CONFERENCE ON TRANSPORTATION AND TRAFFIC ENGINEERING (ICTTE 2018), 2018, : 291 - 295
[39] Mechanical Design and Numerical Analysis of a New Front Wing for a Formula One Vehicle
Laguna-Canales, Aldo Saul
Urriolagoitia-Sosa, Guillermo
Romero-Angeles, Beatriz
Martinez-Mondragon, Miguel
Garcia-Laguna, Miguel Angel
Correa-Corona, Martin Ivan
Maya-Anaya, Daniel
Urriolagoitia-Calderon, Guillermo Manuel
FLUIDS, 2023, 8 (07)
[40] A quasi-steady numerical modeling of wake capture for a hovering flapping wing
Zaree, Amir Hossein
Djavareshkian, Mohammad Hassan
INTERNATIONAL JOURNAL OF MODERN PHYSICS C, 2024, 35 (05):

← 1 2 3 4 5 →