首页> 美国政府科技报告 >Model Preparation Area for High Reynolds Number Propulsion Airframe Integration Testing at the National Transonic Facility.

【24h】

Model Preparation Area for High Reynolds Number Propulsion Airframe Integration Testing at the National Transonic Facility.

机译：国家跨音速设施高雷诺数推进机体一体化试验模型准备区。

获取原文

页面导航

摘要
著录项
相似文献
相关主题

摘要

No abstract available

著录项

作者
Jones, G. S.; Flamm, J. D.; Acheson, M. J.; Hudgins, R. C.;
展开▼
作者单位

展开▼
年度 2016
页码 1-22
总页数 22
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
High reynolds number; Transonic wind tunnels; Active control; Calibrating; Flow distribution; Fluid dynamics; Momentum; Industries; Test chambers;

机译：高雷诺数;跨音速风洞;主动控制;校准;流量分布;流体动力学;动量;工业;试验室;
入库时间 2022-08-29 10:46:16

相似文献

外文文献
中文文献
专利

1. Comparison of the NASA Common Research Model European Transonic Wind Tunnel test data to NASA National Transonic Facility test data [J] . Melissa Rivers, Jürgen Quest, Ralf Rudnik CEAS Aeronautical Journal . 2018,第2期

机译：NASA通用研究模型欧洲跨音速风洞测试数据与NASA国家跨音速设施测试数据的比较
2. Combined-Wedge Waverider for Airframe–Propulsion Integration [J] . Hu Shuyao, Jiang Chongwen, Gao Zhenxun, AIAA Journal . 2018,第8期

机译：组合楔形波乘器，用于飞机推进系统
3. Airframe integration for an LH2 hybrid-electric propulsion system [J] . Howard Smith Aircraft engineering . 2014,第6期

机译：LH2混合动力推进系统的机身集成
4. Model Preparation Areas for Propulsion Airframe Integration Testing at the NASA Langley Research Center [C] . Gregory S. Jones, Donald R. Saxer, Jeffrey D. Flamm AIAA SciTech Forum and Exposition . 2021

机译：NASA Langley研究中心推进机构集成测试的模型准备领域
5. Design, Fabrication, Performance Testing, and Modeling of Diffusion Bonded Compact Heat Exchangers in a High-Temperature Helium Test Facility. [D] . Mylavarapu, Sai K. 2011

机译：高温氦气测试设施中扩散键合紧凑型换热器的设计，制造，性能测试和建模。
6. SPARSE—A subgrid particle averaged Reynolds stress equivalent model: testing with a priori closure [O] . Sean L. Davis, Gustaaf B. Jacobs, Oishik Sen, -1

机译：SPARSE-亚网格平均雷诺应力等效模型：先验封闭测试
7. A Proposal for Integration of Wind Tunnel and Engine Test Programs for the Evaluation of Airframe-Propulsion Compatibility Using Numerical Simulations [O] . Milt Davis, William Baker, Greg Power, 1999

机译：使用数值模拟将风洞和发动机测试程序集成的建议，用于评估机身推进性兼容性

Model Preparation Area for High Reynolds Number Propulsion Airframe Integration Testing at the National Transonic Facility.

摘要

著录项

相似文献

相关主题

期刊订阅