Results 131 to 140 of about 2,515 (186)
Some of the next articles are maybe not open access.
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.
openaire +1 more source
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.
openaire +1 more source
Will there or will there not be a hypersonic airplane?
Journal of Engineering Physics and Thermophysics, 2000An analytical overview of the problems of heat transfer occurring in horizontal flight of a body in the earth’s atmosphere at a hypersonic speed is given. It is shown that, despite the enormous experience accumulated in the design and development of shuttle systems (Space Shuttle, Buran), the creation of a hypersonic airplane still remains a serious ...
openaire +1 more source
2015
Abstract The chapter starts its analysis with blunt-nosed bodies. In a supersonic flow, a blunt-nosed body produces a bow shock wave. The chapter shows that the shape of the shock and the entire flow between the shock and the body become independent of the Mach number, M∞, provided it is large enough.
openaire +1 more source
Abstract The chapter starts its analysis with blunt-nosed bodies. In a supersonic flow, a blunt-nosed body produces a bow shock wave. The chapter shows that the shape of the shock and the entire flow between the shock and the body become independent of the Mach number, M∞, provided it is large enough.
openaire +1 more source
Review of control and guidance technology on hypersonic vehicle
Chinese Journal of Aeronautics, 2022Xiaokui Yue +2 more
exaly
Analysis of Associative Ionization Rates for Hypersonic Flows
Journal of Thermophysics and Heat Transfer, 2021Iain Boyd, Eswar Josyula
exaly
INTERACTIONS BETWEEN A HYPERSONIC WAKE AND A FOLLOWING HYPERSONIC PROJECTILE
AIAA Journal, 1963R. E. SLATTERY +2 more
openaire +1 more source
Wall Pressure Fluctuations Beneath Hypersonic Boundary Layer over Plate
AIAA Journal, 2021Xiaojian Zhao
exaly
Research progress on active thermal protection for hypersonic vehicles
Progress in Aerospace Sciences, 2020Wen Bao, Yu Feng, Jingying Zuo
exaly
Review of acoustic metasurfaces for hypersonic boundary layer stabilization
Progress in Aerospace Sciences, 2022Juanmian Lei, Chih-Yung Wen, Rui Zhao
exaly