Results 131 to 140 of about 2,480 (186)

Hypersonic Flows

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

Hypersonic wakes

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

Review of control and guidance technology on hypersonic vehicle

Chinese Journal of Aeronautics, 2022
Xiaokui Yue, Yibo Ding, Guangshan Chen   +2 more
exaly  

Review of acoustic metasurfaces for hypersonic boundary layer stabilization

Progress in Aerospace Sciences, 2022
Juanmian Lei, Chih-Yung Wen, Rui Zhao
exaly  

Autonomy for Hypersonics.

Proposed for presentation at the Hypersonic Weapons Summit (VIRTUAL) in ,, 2021
openaire   +1 more source

Sublimation in a Hypersonic Environment

Journal of the Aerospace Sciences, 1960
openaire   +2 more sources

Research progress on active thermal protection for hypersonic vehicles

Progress in Aerospace Sciences, 2020
Silong Zhang, Wen Bao, Yu Feng
exaly  

HYPERSONIC AREA RULE

AIAA Journal, 1963
openaire   +1 more source

Hypersonic Flows

2021
openaire   +1 more source

Review of combustion stabilization for hypersonic airbreathing propulsion

Progress in Aerospace Sciences, 2020
Damiano Baccarella, Qili Liu, Tonghun Lee   +2 more
exaly