首页> 美国政府科技报告 >Investigation of a digital simulation of the XB-70 inlet and its application to flight- experienced free-stream disturbances at Mach numbers of 2.4 to 2.6

【24h】

Investigation of a digital simulation of the XB-70 inlet and its application to flight- experienced free-stream disturbances at Mach numbers of 2.4 to 2.6

机译：研究XB-70进气道的数字仿真及其在飞行经历的自由流扰动中的应用，马赫数为2.4至2.6

获取原文

页面导航

摘要
著录项
相似文献
相关主题

摘要

Digital simulation program to predict atmospheric turbulence effects on inlet system of XB-70 aircraft

著录项

作者
Gallagher, R. J.;
展开▼
作者单位

展开▼
年度 1970
页码 1-28
总页数 28
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
ATMOSPHERIC TURBULENCE; B-70 AIRCRAFT; DIGITAL SIMULATION; ENGINE INLETS; FREE FLOW; INLET PRESSURE;

机译：大气湍流; B-70飞机;数字仿真;发动机进气;自由流动;进口压力;

相似文献

外文文献
中文文献
专利

1. Numerical investigations of transition between regular and Mach reflections caused by free-stream disturbances [J] . Kudryavtsev A., Khotyanovsky DV., Ivanov MS., Shock Waves . 2002,第2期

机译：自由流扰动引起的正反射与马赫反射之间过渡的数值研究
2. Numerical simulations of the flow through the inlet and isolator of a Mach 4 dual mode scramjet [J] . S. Janarthanam, V. Babu The Aeronautical Journal . 2012,第1182期

机译：通过Mach 4双模超燃冲压发动机进气口和隔离器的流动的数值模拟
3. Combined free-stream disturbance measurements and receptivity studies in hypersonic wind tunnels by means of a slender wedge probe and direct numerical simulation [J] . AlexanderWagner, ErichSchülein, RenéPetervari, Journal of Fluid Mechanics . 2018,第期

机译：通过细长的楔探测和直接数值模拟，在超音速风隧道中混合在超声波风隧道中的综合扰动测量和接收性研究
4. Investigations on effects of free-stream mach numerber on flow and aeroacoustic characteristics in cavity [C] . Yang Dang-guo, Liang Jin-min, Li Jian-qiang, Proceedings of the 2010 Symposium on Piezoelectricity, Acoustic Waves and Device Applications . 2010

机译：自由流马赫数对空腔流动和空气声特性的影响研究
5. Investigation of side wall effects on an inward scramjet inlet at Mach number 8.6. [D] . Rolim, Tiago Cavalcanti. 2013

机译：研究马赫数为8.6时向内超燃冲压进气口的侧壁效应。
6. Tandem Mach Zehnder Directional Coupler Design and Simulation on Silicon Platform for Optical Coherence Tomography Applications [O] . Yi-Ting Lu, Benedictus Yohanes Bagus Widhianto, Shih-Hsiang Hsu, 2020

机译：用于光学相干层析成像应用的硅平台串联Mach Zehnder定向耦合器设计和仿真
7. Reynolds Number and Cowl Position Effects for a Generic Sidewall Compression Scramjet Inlet at Mach 10: A Computational and Experimental Investigation [O] . Holland Scott D. 1992

机译：通用侧壁压缩超燃冲压发动机进气口在10马赫时的雷诺数和风帽位置影响：计算和实验研究
8. Investigation of a Digital Simulation of the Xb-70 Inlet and Its Application to Flight- Experienced Free-Stream Disturbances at Mach Numbers of 2.4 to 2.6 [R] . Gallagher, R. J. 1970

机译：Xb-70进气道数字仿真研究及其在马赫数为2.4至2.6的飞行经验自由流扰动中的应用

Investigation of a digital simulation of the XB-70 inlet and its application to flight- experienced free-stream disturbances at Mach numbers of 2.4 to 2.6

摘要

著录项

相似文献

相关主题

期刊订阅