首页> 外文会议>24th Applied Aerodynamics Conference >Improved Transonic Wing Flow Calculations Using Transition Correlations

【24h】

Improved Transonic Wing Flow Calculations Using Transition Correlations

机译：利用过渡相关性改进的跨音速翼流计算

获取原文

页面导航

著录项
相似文献
相关主题

著录项

来源
《24th Applied Aerodynamics Conference》|2006年|P.1-8|共8页
会议地点 San Francisco CA(US)
作者
E. G?;
展开▼
作者单位

?rdamar, R. ??ete, and H. Aksel, Middle East Technical University, Ankara, Turkey;

展开▼
会议组织
原文格式 PDF
正文语种
中图分类空气动力学;
关键词

相似文献

外文文献
中文文献
专利

1. Fully Three-Dimensional Transition Prediction on Swept Wings in Transonic Flows [J] . Marc Langlois, Christian Masson, Ion Paraschivoiu Journal of Aircraft . 1998,第2期

机译：跨音速流扫掠机翼的全三维过渡预测
2. Direct Numerical Simulation of the Three-Dimensional Transition to Turbulence in the Transonic Flow around a Wing [J] . S. Bourdet, A. Bouhadji, M. Braza, Flow, turbulence and combustion . 2003,第1a4期

机译：机翼周围跨音速流向湍流的三维过渡的直接数值模拟
3. Correlation-Based Transition Model for Swept-Wing Flow Using the Cross-Flow Reynolds Number [J] . Zhang Wen, Liu Peiqing, Guo Hao Journal of Aircraft . 2017,第1期

机译：基于关联流的雷诺数横掠流的过渡模型
4. Improved Transonic Wing Flow Calculations Using Transition Correlations [C] . Applied Aerodynamics Conference . 2006

机译：使用转换相关性改进的横跨翼流计算
5. The Use of Separation Induced Laminar to Turbulent Flow Transition to Improve the Performance and Robustness of Low Reynolds Numbers Airfoils and Wings [D] . Di Luca, Matteo. 2021

机译：使用分离诱导的层流到湍流过渡，提高低雷诺数翼型和翼的性能和鲁棒性
6. Dosimetrical and radiobiological approach to manage the dosimetric shift in the transition of dose calculation algorithm in radiation oncology: how to improve high quality treatment and avoid unexpected outcomes? [O] . Abdulhamid Chaikh, Jarkko Ojala, Catherine Khamphan, 2018

机译：剂量和放射生物学方法来管理放射肿瘤学中剂量计算算法过渡中的剂量学偏移：如何改善高质量治疗并避免意外结果？
7. Hybrid 3-D Euler/Navier-Stokes calculations of transonic vortex flows over the NTF delta wing [O] . Becker Todd M 1989

机译：混合3-D Euler / Navier-stokes计算跨越NTF三角翼的跨音速涡流
8. The transonic characteristics of a low-aspect-ratio triangular wing with a constant-chord flap as determined by wing-flow tests, including correlation with large-scale tests [R] . Rathert, George A , Jr, Rolls, L Stewart, Hanson, Carl M 1950

机译：通过机翼流动测试确定的具有恒定弦翼的低纵横比三角翼的跨音速特性，包括与大规模试验的相关性

获取原文

客服邮箱：kefu@zhangqiaokeyan.com

京公网安备：11010802029741号 ICP备案号：京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有

客服微信
服务号