Results 91 to 100 of about 330,826 (219)
Combined electric applications in transport [PDF]
Maximizing the efficiency in transport vehicles will be a necessity. This may be realized by introducing a power electronic conversion between the Internal Combustion Engine (ICE) and the wheels. Hence the ICE may be used at its maximal efficiency point.
Van den Bossche, Alex
core +1 more source
A micro-pulse detonation engine (μPDE) was designed and installed to a direct-connect scramjet combustor of Pusan National University (PNU-DCSC). The active excitation on the scramjet combustor was experimentally studied using the μPDE operating at ...
Keon-Hyeong Lee +3 more
doaj +1 more source
Effect of flame-tube head structure on combustion chamber performance [PDF]
The experimental combustion performance of a premixed, pilot-type flame tube with various head structures is discussed. The test study covers an extensive area: efficiency of the combustion chamber, quality of the outlet temperature field, limit of the ...
Gu, Minqqi
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The spray and combustion characteristics of a gas-centered swirl coaxial (GCSC) injector used in oxidizer-rich staged combustion cycle engines were analyzed.
Jungho Lee +4 more
doaj +1 more source
Simulation studies of combustion in a constant-mass variable-volume combustion chamber [PDF]
A numerical simulation code was used to conduct a systematic study of the effects of fuel-air equivalence ratios in the range 0.7 ≤ φ ≤ 1.4 and compression ratio, rc = 8.0 on key operating parameters, such as pressure, rate of change of pressure, '/dt ...
Anetor Lucky, Osakue Edward E.
doaj
Experimental investigation of a swept-strut fuel-injector concept for scramjet application [PDF]
Results are presented of an experiment to investigate the behavior at Mach 4 flight conditions of the swept-strut fuel-injector concept employed in the Langley integrated modular scramjet engine design.
Anderson, G. Y. +3 more
core +1 more source
Preliminary tests of an advanced high-temperature combustion system [PDF]
A combustion system has been developed to operate efficiently and with good durability at inlet pressures to 4.05 MPa (40 atm), inlet air temperatures to 900 K, and exhaust gas temperatures to 2480 K.
Jacobs, R. E. +3 more
core +1 more source
This study investigated combustion characteristics of composite fuel grains designed based on a modular fuel unit strategy. The modular fuel unit comprised a periodical helical structure with nine acrylonitrile–butadiene–styrene helical blades.
Junjie Pan +6 more
doaj +1 more source
Effect of model selection on combustor performance and stability predictions using ROCCID [PDF]
The ROCket Combustor Interactive Design (ROCCID) methodology is an interactive computer program that combines previously developed combustion analysis models to calculate the combustion performance and stability of liquid rocket engines.
Giuliani, James E., Klem, Mark D.
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Influence of water content in ethanol-water blends on the performance and emissions of an SI engine [PDF]
C
Casier, Ben +4 more
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