Results 151 to 160 of about 22,484 (217)

Effects of Wall Temperature on Scalar and Turbulence Statistics During Premixed Flame-Wall Interaction Within Turbulent Boundary Layers. [PDF]

Flow Turbul Combust
Ghai SK, Ahmed U, Chakraborty N.
europepmc   +1 more source

Numerical investigation of low-frequency shock train oscillations in a divergent isolator with vortex generator jets. [PDF]

PLoS One
Wang J, He K, Zhou Q, Wang J.
europepmc   +1 more source

Spectrally Resolved Visible–Near Infrared Radiation in Swirl Combustors

Hyunseung Rhee, Wonjik Shin, Jaekun Lee, Kyeongsun Kim, Youchan Park, Hosung Byun, Hyungrok Do   +6 more
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Laser ablation ignition modes in a cavity-based supersonic combustor

Jianheng Ji, Zun Cai, Taiyu Wang, Yifu Tian, Mingbo Sun, Jiajian Zhu, Zhenguo Wang   +6 more
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Numerical Investigation of Reacting Flows in Gas Turbine Model Combustors

, 2018
Andreas Fiolitakis, Christian Eberle, Martin Grader   +2 more
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Effects of Combustor Enclosure Flow Path on Combustor Design

Volume 4A: Combustion, Fuels, and Emissions, 2020
Abstract A design optimization procedure was implemented to resize the holes of a combustor liner for practical applications. A combustor geometry evaluated without an enclosure was to be reformulated within an enclosure. The objective functions of the combustor with enclosure involved targeting the flow splits of the combustor without ...
Alejandro M. Briones, Nathan Thomas, Brent A. Rankin   +2 more
openaire   +1 more source

Reynolds analogy in combustor modeling

International Journal of Heat and Mass Transfer, 2007
Accurate temperature prediction is vital for the development of advanced combustion systems. The Reynolds analogy concept has been almost exclusively used in current turbulent reacting flow RANS simulations. In this paper, this hypothesis applied to a diffusion flame model combustor is discussed and assessed. Some of the numerical results obtained from
Jiang, L. Y., Campbell, I.
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One-dimensional combustor optimization.

Journal of Spacecraft and Rockets, 1968
The steepest-descent optimization technique has been applied to the equations describing the steady one-dimensional flow process with heat addition. Using a simplified kinetic model for the H2-air combustion process, the effects of mixing, friction, and shock total pressure losses are simulated.
A. BRANDT, L. PERINI
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Compressor/Diffuser/Combustor Aerodynamic Interactions in Lean Module Combustors

Journal of Engineering for Gas Turbines and Power, 2007
The paper reports an experimental investigation into the possibility of increased interactions between combustor external aerodynamics and upstream components, e.g., prediffuser, compressor outlet guide vane (OGV), and even the compressor rotor, caused by the trend in lean module fuel injectors to larger mass flows entering the combustor cowl.
A. Duncan Walker, Jon F. Carrotte, James J. McGuirk   +2 more
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The pressurized combustor

1995
Process considerations such as fluidization mode and steam cycle dictate how the pressurized combustor is configured. The impact of these process parameters on combustor configuration are addressed in the following sections.
S. J. Goidich, A. Robertson
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