首页> 外文会议>AIAA Aerospace Sciences Meeting and Exhibit >An Engineering Inviscid- Reacting Boundary Layer Method for Calculation of Hypersonic Aerodynamic Heating

【24h】

An Engineering Inviscid- Reacting Boundary Layer Method for Calculation of Hypersonic Aerodynamic Heating

机译：高超声速空气动力加热的工程无粘边界层计算方法

获取原文

页面导航

著录项
相似文献
相关主题

著录项

来源
《AIAA Aerospace Sciences Meeting and Exhibit》|2005年|P.1-9|共9页
会议地点
作者
A. Najafiyazdi;
展开▼
作者单位

展开▼
会议组织
原文格式 PDF
正文语种
中图分类航空;
关键词

相似文献

外文文献
中文文献
专利

1. A hypersonic aeroheating calculation method based on inviscid outer edge of boundary layer parameters [J] . Meng ZhuXuan, Fan Hu, Peng Ke, Acta astronautica . 2016,第deca期

机译：基于边界层参数无粘性外边缘的高超音速空气加热计算方法
2. Aerodynamic heating in transitional hypersonic boundary layers: Role of second-mode instability [J] . Zhu Yiding, Chen Xi, Wu Jiezhi, Physics of fluids . 2018,第1期

机译：过渡超声边界层的空气动力学加热：第二模式不稳定的作用
3. Surface Heating and Boundary-Layer Transition on a Hypersonic Inflatable Aerodynamic Decelerator [J] . Hollis Brian R. Journal of Spacecraft and Rockets . 2018,第4期

机译：高超声速充气减速器的表面加热和边界层过渡
4. An Engineering Inviscid- Reacting Boundary Layer Method for Calculation of Hypersonic Aerodynamic Heating [C] . American Institute of Aeronautics and Astronautics Aerospace Sciences Meeting and Exhibit . 2005

机译：高超声波空气动力加热计算的工程活性反应边界层方法
5. INTEGRAL METHODS IN COMPRESSIBLE LAMINAR BOUNDARY LAYERS AND THEIR APPLICATION TO HYPERSONIC PRESSURE INTERACTION. [D] . CHAN, YAT-YUNG. 1965

机译：可压缩层流边界层中的积分方法及其在超音速压力相互作用中的应用。
6. Effect of a Roughness Element on the Hypersonic Boundary Layer Receptivity Due to Different Types of Free-Stream Disturbance with a Single Frequency [O] . Mingfang Shi, Lidan Xu, Zhenqing Wang, 2019

机译：粗糙元件对超声边界层接收性的影响由于单频带不同类型的自由流扰动
7. Aerodynamic Heating of a Gap in the Hypersonic Laminar Boundary Layer [O] . Hironao YOKOI, Hiroto KOYAMA, Yoshiaki NAKAMURA 2013

机译：超声波层边界层中间隙的空气动力学加热

An Engineering Inviscid- Reacting Boundary Layer Method for Calculation of Hypersonic Aerodynamic Heating

著录项

相似文献

相关主题

期刊订阅