Results 181 to 190 of about 22,114 (235)
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1962
An experimental investigation was made of the flow field behind a two-dimensional circular cylinder at a nominal Mach number of 5.7. The free-stream Reynolds number based on the cylinder diameter was varied over a range from 4300 to 66, 500 by changing both the diameter of the cylinder and the stagnation pressure of the wind tunnel.
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An experimental investigation was made of the flow field behind a two-dimensional circular cylinder at a nominal Mach number of 5.7. The free-stream Reynolds number based on the cylinder diameter was varied over a range from 4300 to 66, 500 by changing both the diameter of the cylinder and the stagnation pressure of the wind tunnel.
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Review of control and guidance technology on hypersonic vehicle
Chinese Journal of Aeronautics, 2022Yibo Ding, Guangshan Chen
exaly
Review of acoustic metasurfaces for hypersonic boundary layer stabilization
Progress in Aerospace Sciences, 2022Rui Zhao, Chih-Yung Wen, Guohua Tu
exaly
Proposed for presentation at the Hypersonic Weapons Summit (VIRTUAL) in ,, 2021
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Research progress on active thermal protection for hypersonic vehicles
Progress in Aerospace Sciences, 2020Silong Zhang, Jingying Zuo, Jiang Qin
exaly
Review of combustion stabilization for hypersonic airbreathing propulsion
Progress in Aerospace Sciences, 2020Qili Liu +2 more
exaly
Laser ablation behavior of C/SiC composites subjected to transverse hypersonic airflow
Corrosion Science, 2021Hongwei Song, Wu Yuan, Yuwen Liu
exaly
Sublimation in a Hypersonic Environment
Journal of the Aerospace Sciences, 1960openaire +2 more sources