Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Cetera Chen"'
Publikováno v:
ACS Omega, Vol 8, Iss 49, Pp 47075-47085 (2023)
Externí odkaz:
https://doaj.org/article/09c5fe416e5a4115ae68ff9338169351
Publikováno v:
SSRN Electronic Journal.
Autor:
Cheng-Hsien Shen, Wilson Chen, Yu-Cheng Chang, Hsiu-Hsia Lee, Eric Wang, Cetera Chen, Kuo-En Huang
Publikováno v:
Energy & Fuels. 32:3660-3667
The Industrial Technology Research Institute has developed a 30 kWth moving bed chemical looping system for hydrogen production. Methane is supplied as a fuel to the reducer, and steam is supplied to the oxidizer to produce hydrogen. An iron-based ox
Publikováno v:
Journal of Propulsion and Power. 27:509-512
T HE miniaturization of space systems, such as microsatellites, has become an important development trend. Using a cluster of microspacecraft with a constellational architecture to replace a traditional spacecraft can greatly reduce the costs of prod
Publikováno v:
AIAA Journal. 47:2359-2367
The combustion phenomena of doublet impingements of nitrogen tetroxide and monomethylhydrazine were observed in this research. The total flow rates of the propellants were controlled at 8:00 g=s to simulate the operation of a 5 lbf rocket, and the ra
Publikováno v:
AIAA Journal. 44:2259-2266
The spray phenomena of doublet and triplet impingements of nitrogen tetroxide (NTO) and monomethylhydrazine (MMH) simulants were studied by the planar laser induced fluorescence technique. The total flow rates of the simulants were controlled at ∼8
Publikováno v:
AIAA Journal. 39:1123-1126
Supersonic flows past a blunt body in air and in water are numerically investigated by using a high-resolution Euler/Navier-Stokes solver. The numerical method used is a fourth-order Runge-Kutta method for time integration with a fifth-order weighted
Publikováno v:
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
By the PLIF optical technique, this study focused on the development of the impinging type injector design of the 100-lbf level monomethylhydrazine/nitrogen tetroxide liquid rocket. The design of the multi-pair impinging injector plate is based on th
Publikováno v:
45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Publikováno v:
45th AIAA Aerospace Sciences Meeting and Exhibit.
[Abstract] The combustion phenomena of doublet impingements of nitrogen tetroxide (NTO) and monomethylhydrazine (MMH) were studied in this research. The total flow rates of the propellants were controlled at ~8.00 g/s to simulate the operation of a 5