首页> 外文OA文献 >COMPUTATION OF WALL HEAT FLUXES IN HYPERSONIC INLET FLOWS

【2h】

COMPUTATION OF WALL HEAT FLUXES IN HYPERSONIC INLET FLOWS

机译：超音速进气流中壁面热通量的计算

页面导航

著录项
相似文献
相关主题

著录项

作者
Birgit U. Reinartz; Jörn Van Keuk; Turan Coratekin; Josef Ballmann;
展开▼
作者单位

展开▼
年度 2002
总页数
原文格式 PDF
正文语种
中图分类

相似文献

外文文献
中文文献
专利

1. COMPUTATION OF HEAT FLUX IN HYPERSONIC FLOW WITH A CARTESIAN MESH USING NEAR-WALL RESOLUTION [J] . V. Ashok, George Joseph, V. Adimurthy Journal of Aerospace Sciences and Technologies . 2013,第2期

机译：近壁解析法用笛卡尔网格法计算渗流中的热通量
2. Correlation Analysis of Separation Shock Oscillation and Wall Pressure Fluctuation in Unstarted Hypersonic Inlet Flow [J] . Chengpeng Wang, Xin Yang, Longsheng Xue, Aerospace . 2019,第1期

机译：未启流超声入口流动分离冲击振荡和壁压波动的相关分析
3. A low-computational-cost inverse heat transfer technique for convective heat transfer measurements in hypersonic flows [J] . Avallone F., Greco C. S., Schrijer F. F. J., Experiments in Fluids: Experimental Methods and Their Applications to Fluid Flow . 2015,第4期

机译：一种低计算成本的逆传热技术，用于高超声速流中的对流传热测量
4. Sensitivity of Heat Fluxes in Hypersonic CO_2 Flows to the State-to-state Kinetic Schemes [C] . I. Armenise, E. Kustova International Symposium on Rarefied Gas Dynamics . 2016

机译：超声波CO_2在高温助熔剂中的敏感性流到状态到状态动力学方案
5. EFFECT OF SPATIALLY PERIODIC HEATING OR AN ABRUPT CONTRACTION AT INLET ON TRANSITIONAL AND TURBULENT HEAT TRANSFER IN A DUCT (UNSYMMETRIC, INTERRUPTED WALL CONDITIONS, SEPARATED FLOWS, ENHANCED, FORWARD STEP). [D] . GARCIA GUTIERREZ, ALFONSO. 1985

机译：入口处的周期性周期性加热或突然压缩对管道中的过渡和湍流传热的影响（不对称，壁面中断的条件，单独的流动，增强的，向前的步骤）。
6. Effects of two-phase inlet quality mass velocity flow orientation and heating perimeter on flow boiling in a rectangular channel: Part 1 – Two-phase flow and heat transfer results [O] . Chirag R. Kharangate, Lucas E. O’Neill, Issam Mudawar -1

机译：两相入口质量质量速度流向和加热周长对矩形通道中流沸腾的影响：第1部分–两相流和传热结果
7. Two- and three-dimensional viscous computations of a hypersonic inlet flow [O] . Kunik William G., Taylor Arthur, Benson Thomas J., 1987

机译：高超声速入口流的二维和三维粘性计算
8. Time Accurate Computation of Unsteady Hypersonic Inlet Flows with a Dynamic FlowAdaptive Mesh [R] . McRae, D. S., Neaves, M. 1998

机译：用动态流动自适应网格计算非定常高超声速进气流的时间精度

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