俄罗斯空气动力研究所中心学报
每年出版 6 期
ISSN 打印: 1948-2590
ISSN 在线: 1948-2604
ALGORITHM FOR GENERATING SWEPT VOLUME MESHES NEAR AN AIRCRAFT WING
卷 43,
册 1, 2012,
pp. 87-100
DOI: 10.1615/TsAGISciJ.2012005305
摘要
An algorithm for generating swept volume meshes using an input mapped guide and unstructured cross surface meshes is presented. The algorithm usage is illustrated with an example of mesh generation near an aircraft wing with a slat and flap deflected for landing.
参考文献
-
Khitryh, D., Survey of advanced possibilities of mesh generator ICEM CFD.
-
Khitryh, D., Survey of advanced possibilities of mesh generator ICEM CFD, Part 2.
-
Yurchenko, D., Numerical simulation of flow in vortex tube using ANSYS Fluent.
对本文的引用
-
Ryabinin Anatoly, Calculation of transonic flow past the twisted wings, 2015 International Conference on Mechanics - Seventh Polyakhov's Reading, 2015. Crossref
301 文章浏览量
14 文章下载
统计数据
相似内容的文章:
最新一期
KIRILL IVANOVICH SYPALO−50TH ANNIVERSARY
NUMERICAL STUDY OF THE DISTURBANCES GENERATED BY MICROJETS IN A SUPERSONIC FLAT-PLATE BOUNDARY LAYER
ANALYSIS OF THE MOVING DETONATION INTERACTION WITH TURBULENT BOUNDARY LAYERS IN A DUCT ON THE BASIS OF NUMERICAL SIMULATION
EXPERIMENTAL STUDY OF COUNTERFLOW BLOWING IN HIGH-SPEED FLOW THROUGH AN ASYMMETRIC SLOT IN THE LEADING EDGE OF A SHARP WEDGE
ASYMPTOTIC SOLUTIONS TO HYPERSONIC BOUNDARY LAYER EQUATIONS ON A FLAT WING WITH A POINT OF INFLECTION ON THE LEADING EDGE
WAVE MODEL OF ORGANIZED STRUCTURES IN A TURBULENT BOUNDARY LAYER ON A PLATE WITH ZERO LONGITUDINAL PRESSURE GRADIENT
NUMERICAL SIMULATION OF THE FLOW AROUND LANDSCAPE FRAGMENTS AND SOLUTION VERIFICATION
POLYNOMIAL REPRESENTATION OF THERMODYNAMIC PROPERTIES OF COMBINED FUEL SYSTEMS IN RAMJET SIMULATION MODELS
A MODEL TEST METHODOLOGY FOR THE INVESTIGATION OF AN ELASTICALLY SCALED MAIN ROTOR
INDEX, VOLUME 51, 2020