首页> 美国政府科技报告 >Some experiments at high supersonic speeds on the aerodynamic and boundary-layer transition characteristics of high-drag bodies of revolution

【24h】

Some experiments at high supersonic speeds on the aerodynamic and boundary-layer transition characteristics of high-drag bodies of revolution

机译：一些高超音速速度的实验对高阻力旋转体的空气动力学和边界层过渡特性

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
Seiff, Alvin; Sommer, Simon C; Canning, Thomas N;
展开▼
作者单位

展开▼
年度 1957
页码 1-94
总页数 94
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词

相似文献

外文文献
中文文献
专利

1. Minimization of body of revolution aerodynamic drag at supersonic speeds [J] . Ageev Nikita, Pavlenko Alexander Aircraft engineering . 2016,第2期

机译：以超音速降低旋转体的空气阻力
2. EFFECT OF DISTRIBUTED GAS INJECTION ON AERODYNAMIC CHARACTERISTICS OF A BODY OF REVOLUTION IN A SUPERSONIC FLOW [J] . V. M. Fomin, V. I. Zapryagaev, A. V. Lokotko, Journal of Applied Mechanics and Technical Physics . 2012,第3期

机译：分布气体喷射对超声速旋转体气动特性的影响
3. Aerodynamic Characteristics of Bodies of Revolution at Near-Sonic Speeds [J] . Brenda M. Kulfan, John E. Bussoletti, Craig L. Hilmes Journal of Aircraft . 2007,第6期

机译：接近声速的旋转机构的空气动力学特性
4. BOUNDARY-LAYER TRANSITION MEASUREMENTS ON AN AXISYMMETRIC BODY AT INCIDENCE AT SUPERSONIC SPEED [C] . . 2004

机译：超声速入射时轴对称物体的边界层过渡测量
5. THE INFLUENCE OF ARTIFICIALLY INDUCED TURBULENCE UPON BOUNDARY-LAYER TRANSITION IN SUPERSONIC FLOWS. [D] . OLSON, LAWRENCE ELROY. 1970

机译：人工感应湍流对边界层过渡在超声速流动中的影响。
6. Aerodynamic Characteristics of a Stoker Furnace withStaged Combustion: Comparison of Cold Modeling Experiments and NumericalSimulations [O] . Xinwei Guo, Hao Bai, Zhongxiao Zhang, 2020

机译：炉膛空气动力学特性分阶段燃烧：冷建模实验与数值比较模拟
7. EFFECT OF BODY SHAPE ON THE AERODYNAMICS OF PROJECTILES AT SUPERSONIC SPEEDS [O] . ABDULKAREEM SH. MAHDI, MUSHTAK AL-ATABI 2008

机译：体形对超速速下弹丸气动的影响

Some experiments at high supersonic speeds on the aerodynamic and boundary-layer transition characteristics of high-drag bodies of revolution

摘要

著录项

相似文献

相关主题

期刊订阅