CORRECTIONS

作品数：162被引量：148H指数：6
导出分析报告
相关领域：理学更多>>
相关作者：樊莹莹程山李媛媛赵云辉肖振军更多>>
相关机构：西北民族大学西南大学邵阳学院南京师范大学更多>>
相关期刊：更多>>
相关基金：国家自然科学基金国家重点基础研究发展计划国家高技术研究发展计划中国博士后科学基金更多>>
-
在结果中检索

检索结果分析

结果分析中...
选择条件：
  • 期刊=Chinese Journal of Aeronauticsx
共 条 记 录，以下是1-4
全选清除导出
参考文献引证文献引用追踪
视图：
排序：
Assessment of Two Turbulence Models and Some Compressibility Corrections for Hypersonic Compression Corners by High-order Difference Schemes被引量：14
《Chinese Journal of Aeronautics》2012年第1期25-32,共8页TU Guohua DENG Xiaogang MAO Meiliang 
Foundation items： National Basic Research Program of China （2009CB723801）; National Natural Science Foundation of China （11072259）
The Spalart-Allmaras （S-A） turbulence model, the shear-stress transport （SST） turbulence model and their compressibility corrections are revaluated for hypersonic compression comer flows by using high-order differ...
关键词：AERODYNAMICS high-order weighted compact nonlinear scheme hypersonic compression comers turbulence models compressibility corrections shock/boundary layer interactions shock waves 
A Fault-tolerance Estimating Method for Ionosphere Corrections in Satellite Navigation System被引量：2
《Chinese Journal of Aeronautics》2011年第6期749-755,共7页GAO Shuliang LI Rui HUANG Zhigang 
National Basic Research Program of China (2010CB731800)
Aiming to the reliable estimates of the ionosphere differential corrections for the satellite navigation system in the presence of the ionosphere anomaly, a fault-tolerance estimating method, which is based on the dis...
关键词：differential corrections ionosphere anomaly Kalman filter fault-tolerance fault detection 
WALL INTERFERENCE CORRECTIONS FORHIGH-LIFT EXPERIMENT
《Chinese Journal of Aeronautics》1994年第4期256-260,共5页A.Kupper 
in this paper a method is outlined to compute wall-interferenee in closedlow speed wind tunnel for 3D high lift test using wall pressure at optimum points andthe influence function (WPIF method for short). The experim...
关键词：wall pressure INTERFERENCE LIFT low speed subsonic wind tunnels 
TRANSONIC WALL IN TERFERENCE CORRECTIONS FOR CIVIL AIRCRAFT MODEL TESTS
《Chinese Journal of Aeronautics》1994年第3期160-169,共10页Fan Zhaolin Cui Naiming Yun Qilin Yin Lupin(China Aerodynamics Research & Development Center,Mianyang, Sichuan, China, 621000) 
The correction method uses the static pressures measured near the tunnelwalls during model tests as boundary conditions. It is required that the flow near thewalls is subsonic and the freestream Mach number is less th...
关键词：aerodynamic interference transonic wind tunnels wall pressure. data reduction 
全选清除导出
共1页<1>
检索报告 对象比较 聚类工具 使用帮助 返回顶部