Correlation between total pressure losses of highly loaded annular diffusers and integral stage design parameters [PDF]
Journal of the Global Power and Propulsion Society, 2018 Diffusers convert kinetic flow energy into a rise in static pressure. This pressure recovery is the primary aerodynamic design objective for exhaust gas diffusers in power-generating steam and gas turbines. The total pressure loss is an equally important
Dajan Mimic +2 more
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Recovery ... reporting overview; Connecticut recovery; CT recovery ... progress
, 2010 Updated quarterly; Began in 2009.; Title from home page last modified 10/29/2009 (viewed Oct. 29, 2009).; At head of title: State of Connecticut.; "On October 1, state agencies that have received Recovery Act funds began reporting to the federal ...
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Numerical Study on Effects of High-Frequency Arrayed Energy Deposition on Scramjet Combustor Performance [PDF]
Hangkong bingqi, 2023 For the supersonic flows have large momentum, it is difficult to get higher penetration depth because of the influence of transverse jet on incoming flow so as to affect the mixing and combustion efficiency of jet in scramjet combustor.
Cai Zilin, Gao Feng, Wang Hongyu, Ma Cenrui
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Improving the efficiency of a serpentine inlet duct by using of Blowing Jet Vortex Generators flow control technique [PDF]
مجله مدل سازی در مهندسی, 2018 In this research, aerodynamic performance of a double s-shaped serpentine inlet duct is numerically investigated by using of blowing Jet vortex generators flow control technique.
iman Maghsoudi +2 more
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Applied Sciences, 2023 Submerged inlet has been widely used in UAVs and cruise missiles due to its good stealth characteristics, but it also brings the disadvantage of poor aerodynamic characteristics.
Junyao Zhang, Baigang Mi
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Jet Mixings of Alternating-Lobe Nozzles under Pumping Air Intake and Stamping Air Intake Conditions
Aerospace, 2022 Jet mixings of a coplanar alternating-lobe nozzle (CoALN), scarfing alternating-lobe nozzle (ScALN), sword alternating-lobe nozzle (SwALN), and sword and chevron alternating-lobe nozzle (SwChALN) were numerically investigated using three different far ...
Zhiqiang Sheng +3 more
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Recovery ... reporting overview; Connecticut recovery; CT recovery ... progress
, 2011 Updated quarterly; Began in 2009.; Title from home page last modified 10/29/2009 (viewed Oct. 29, 2009).; At head of title: State of Connecticut.; "On October 1, state agencies that have received Recovery Act funds began reporting to the federal ...
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AERODYNAMIC STUDIES IN THE STATIC COMPONENTS OF A CENTRIFUGAL COMPRESSOR STAGE [PDF]
Journal of Mechanical Engineering and Sciences, 2011 Aerodynamic studies in the static components of a centrifugal compressor stage were conducted using the computational fluid dynamics solver FLUENT. For the simulation study, a typical centrifugal compressor stage geometry with a flow coefficient of 0.053
K. Srinivasa Reddy +2 more
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发电技术, 2019 A combined numerical simulation is conducted to couple fluid flow between exhaust hood and last-stage blades of a 600 MW steam turbine using the computational fluid dynamics software CFX.
Lihua CAO, Kai ZHOU, Heyong SI
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Prepositive Synergistic Bulge Design for Improving Aerodynamic Performance of Submerged Inlet
Aerospace, 2023 A submerged inlet has good stealth characteristics and a low external drag, but it also has the disadvantage of low internal flow efficiency. In view of this, a new efficiency enhancement method based on the prepositive synergistic bulge of the inlet’s ...
Xuan Bai, Baigang Mi
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