Zobrazeno 1 - 4
of 4
pro vyhledávání: '"Chen LH(陈立红)"'
Publikováno v:
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference.
A methodology has been devised for the design of the three-dimensional hypersonic inlets with shape transition. This methodology split the objective three dimensional flowfield into a number of stream tubes, each of which has the contraction ratio th
Publikováno v:
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
In this paper, a numerical analysis coupling heat transfers of the combustor internal flow, the coolant flow and the strut wall is developed and applied for the optimization of strut cooling using aviation kerosene as coolant at flow conditions corre
Publikováno v:
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference.
The TDLAS and static pressure were used to investigate the combustion of the excited ethylene jet into the supersonic flow in this article. The jet was from the Hartmann-Sprenger tube, which was put into the traditional jet device. The jet was excite
Publikováno v:
14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference.
The numerical simulation was conducted to investigate three-dimensional sidewall compression scramjet inlet flow fields. The research also looked into the effects of cowl positions and strut thickness. It is noted that flow separation occurs at the s