首页> 美国政府科技报告 >Heat-Transfer and Static Stability Tests of A 7.5-deg Blunt Cone with Roughness Elements and Sonic Jets to Promote Boundary-Layer Transition at Mach Number 10.

【24h】

Heat-Transfer and Static Stability Tests of A 7.5-deg Blunt Cone with Roughness Elements and Sonic Jets to Promote Boundary-Layer Transition at Mach Number 10.

机译：具有粗糙元素和声波喷射的7.5度钝锥的传热和静态稳定性测试以促进10马赫的边界层转变。

获取原文

页面导航

摘要
著录项
引文网络
相似文献
相关主题

摘要

No abstract available.

著录项

作者
carver , d. b. best, j. t. jr;
展开▼
作者单位

展开▼
年度 1978
页码 1-70
总页数 70
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
reentry vehicles; aerothermodynamicswind tunnel tests; wind tunnel models; nose cones; blunt bodies; conical bodies; boundary layer control; boundary layer transition; aerodynamic characteristics; aerodynamic heating; heat transfer; surface roughness; hypervelocity;

机译：再入飞行器;气动热力学风洞试验;风洞模型;鼻锥;钝体;锥体;边界层控制;边界层过渡;气动特性;气动加热;传热;表面粗糙度;超高速;

相似文献

外文文献
中文文献
专利

1. Boundary-Layer Stability Analysis for Stetson's Mach 6 Blunt-Cone Experiments [J] . Jewell Joseph S., Kimmel Roger L. Journal of Spacecraft and Rockets . 2017,第1期

机译：Stetson的6马赫钝角实验的边界层稳定性分析
2. Mach 6 Boundary-Layer Stability Experiments on Sharp and Blunted Cones [J] . Anatoly A. Maslov, Alexander N. Shiplyuk, Dmitry A. Bountin, Journal of Spacecraft and Rockets . 2006,第1期

机译：锋利和钝锥的Mach 6边界层稳定性实验
3. Boundary-layer instability and transition on a flared cone in a Mach 6 quiet wind tunnel [J] . Jerrod Hofferth, William Saric, Joseph Kuehl, International Journal of Engineering Systems Modelling and Simulation . 2013,第1a3期

机译：Mach 6安静风洞中喇叭形锥的边界层不稳定性和过渡
4. Direct Numerical Simulations of laminar-turbulent boundary-layer transition for a blunt cone at Mach 6 [C] . Andrew B. Hartman, Christoph Hader, Hermann F. Fasel AIAA SciTech Forum and Exposition . 2021

机译：马赫6时钝锥体的层压湍流边界层过渡的直接数值模拟
5. Hypersonic boundary-layer transition measurements at Mach 10 on a large seven-degree cone at angle of attack [D] . Moraru, Ciprian G. 2015

机译：在大七度锥面的迎角处以10马赫的高超声速边界层跃迁测量
6. Effect of a Roughness Element on the Receptivity of a Hypersonic Boundary Layer over a Blunt Cone Due to Pulse Entropy Disturbance with a Single Frequency [O] . Zhenqing Wang, Mingfang Shi, Xiaojun Tang, 2018

机译：粗糙元件对钝锥体上超声边界层的接受性的影响由于单频脉冲熵干扰
7. Numerical Investigation of Boundary-Layer Transition for Cones at Mach 3.5 and 6.0 [O] . Laible Andreas Christian 2011

机译：3.5和6.0马赫锥的边界层过渡的数值研究

Heat-Transfer and Static Stability Tests of A 7.5-deg Blunt Cone with Roughness Elements and Sonic Jets to Promote Boundary-Layer Transition at Mach Number 10.

摘要

著录项

引文网络

相似文献

相关主题

期刊订阅