Results 171 to 180 of about 158,007 (340)
Based on actual goaf conditions, a porosity evolution model considering the superimposed effects of stress–temperature–moisture interactions was developed and experimentally validated using a confined fractured coal mass low‐temperature oxidation testing system simulating goaf scenarios.
Boning Jiang+6 more
wiley +1 more source
Performance Analysis of Pulse Detonation Micro Gas Turbines Under Typical Operating Conditions
ABSTRACT Considering the benefits of pulse detonation combustion, including low entropy increase, high cycle thermal efficiency, and self‐pressurization, a performance calculation model for a pulse detonation micro gas turbine was established using methane as fuel. The study primarily investigated the impact of component parameters, ambient conditions,
Weifeng Qin+3 more
wiley +1 more source
MODELING OF FUEL SPRAY CHARACTERISTICS AND DIESEL COMBUSTION CHAMBER PARAMETERS
The computer model for coordination of fuel spray characteristics with diesel combustion chamber parameters has been created in the paper. The model allows to observe fuel sprays develоpment in diesel cylinder at any moment of injection, to calculate ...
G. M. Kukharonak, D. G. Hershan
doaj
Explosion Characteristics of Layered Wood Dust With High Pressure Oxygen
ABSTRACT Dust explosions have been extensively investigated for process safety. This study introduces an explosion mode involving layered wood dust and high‐pressure oxygen. Unlike atmospheric air conditions, layered wood dust can be triggered by weak ignition energy (60 J) in high‐pressure oxygen environments.
Ze He+6 more
wiley +1 more source
Synergistic optimization of combustion chamber design and hydrogen injection strategies for ultra-lean combustion in hydrogen engines. [PDF]
Huang Z+7 more
europepmc +1 more source
Reliability Analysis of a Structural Ceramic Combustion Chamber [PDF]
Jonathan A. Salem+3 more
openalex +1 more source
Hot fire fatigue testing results for the compliant combustion chamber [PDF]
A hydrogen-oxygen subscale rocket combustion chamber was designed incorporating an advanced design concept to reduce strain and increase life. The design permits unrestrained thermal expansion of a circumferential direction and, thereby, provides ...
Jankovsky, Robert S.+2 more
core +1 more source