Log in

Relevant bibliographies by topics / Combustor loading

Contents

Journal articles
Dissertations / Theses
Books
Book chapters
Conference papers
Reports

Academic literature on the topic 'Combustor loading'

Author: Grafiati

Published: 3 June 2025

Last updated: 20 July 2025

Create a spot-on reference in APA, MLA, Chicago, Harvard, and other styles

Select a source type:

Consult the lists of relevant articles, books, theses, conference reports, and other scholarly sources on the topic 'Combustor loading.'

Next to every source in the list of references, there is an 'Add to bibliography' button. Press on it, and we will generate automatically the bibliographic reference to the chosen work in the citation style you need: APA, MLA, Harvard, Chicago, Vancouver, etc.

You can also download the full text of the academic publication as pdf and read online its abstract whenever available in the metadata.

Journal articles on the topic "Combustor loading"

1

Zelina, J., and D. R. Ballal. "Combustor Stability and Emissions Research Using a Well-Stirred Reactor." Journal of Engineering for Gas Turbines and Power 119, no. 1 (1997): 70–75. http://dx.doi.org/10.1115/1.2815564.

Full text

Abstract:

The design and development of low-emissions, lean premixed aero or industrial gas turbine combustors is very challenging because it entails many compromises. To satisfy the projected CO and NOx emissions regulations without relaxing the conflicting requirements of combustion stability, efficiency, pattern factor, relight (for aero combustor), or off-peak loading (for industrial combustor) capability demands great design ingenuity. The well-stirred reactor (WSR) provides a laboratory idealization of an efficient and highly compact advanced combustion system of the future that is capable of yiel

APA, Harvard, Vancouver, ISO, and other styles

2

Sokolov, K. Y., A. G. Tumanovsky, M. N. Gutnik, A. I. Mechanikov, V. P. Reshitko, and M. I. Grinshtein. "Experimental Investigation of GTE-115 Combustor With Premixed Burner Unit." Journal of Engineering for Gas Turbines and Power 116, no. 3 (1994): 547–53. http://dx.doi.org/10.1115/1.2906854.

Full text

Abstract:

The results of experimental investigation of the basic parameters of one-burner, 1/18 sector of a full-scale annular combustor of the “Turboatom” GTE-115 gas turbine unit are presented. Specifics of fuel burnup and formation of toxic pollutants in premixed combustion using a pilot diffusion burner are presented. Generalized dependences of combustor characteristics versus flow parameters and an optimized algorithm of combustor loading are illustrated.

APA, Harvard, Vancouver, ISO, and other styles

3

Kelsall, G. J., M. A. Smith, and M. F. Cannon. "Low Emissions Combustor Development for an Industrial Gas Turbine to Utilize LCV Fuel Gas." Journal of Engineering for Gas Turbines and Power 116, no. 3 (1994): 559–66. http://dx.doi.org/10.1115/1.2906856.

Full text

Abstract:

Advanced coal-based power generation systems such as the British Coal Topping Cycle offer the potential for high-efficiency electricity generation with minimum environmental impact. An important component of the Topping Cycle program is the gas turbine, for which development of a combustion system to burn low calorific value coal derived fuel gas, at a turbine inlet temperature of 1260°C (2300°F), with minimum pollutant emissions, is a key R&D issue. A phased combustor development program is underway burning low calorific value fuel gas (3.6-4.1 MJ/m3) with low emissions, particularly NOx

APA, Harvard, Vancouver, ISO, and other styles

4

Shaikh, Faisal, and Budimir Rosic. "Unsteady phenomena at the combustor-turbine interface." Journal of the Global Power and Propulsion Society 5 (November 23, 2021): 202–15. http://dx.doi.org/10.33737/jgpps/143042.

Full text

Abstract:

The combustor-turbine interface in a gas turbine is characterised by complex, highly unsteady flows. In a combined experimental and large eddy simulation (LES) study including realistic combustor geometry, the standard model of secondary flows in the nozzle guide vanes (NGV) is found to be oversimplified. A swirl core is created in the combustion chamber which convects into the first vane passages. Four main consequences of this are identified: variation in vane loading; unsteady heat transfer on vane surfaces; unsteadiness at the leading edge horseshoe vortex, and variation in the position of

APA, Harvard, Vancouver, ISO, and other styles

5

Chambers, Steven, Horia Flitan, Paul Cizmas, Dennis Bachovchin, Thomas Lippert, and David Little. "The Influence of In Situ Reheat on Turbine-Combustor Performance." Journal of Engineering for Gas Turbines and Power 128, no. 3 (2004): 560–72. http://dx.doi.org/10.1115/1.2135812.

Full text

Abstract:

This paper presents a numerical and experimental investigation of the in situ reheat necessary for the development of a turbine-combustor. The flow and combustion were modeled by the Reynolds-averaged Navier-Stokes equations coupled with the species conservation equations. The chemistry model used herein was a two-step, global, finite rate combustion model for methane and combustion gases. A numerical simulation was used to investigate the validity of the combustion model by comparing the numerical results against experimental data obtained for an isolated vane with fuel injection at its trail

APA, Harvard, Vancouver, ISO, and other styles

6

Miccio, Francesco, Fabrizio Scala, and Riccardo Chirone. "Fluidized Bed Combustion of a Biomass Fuel: Comparison Between Pilot Scale Experiments and Model Simulations." Journal of Heat Transfer 127, no. 2 (2005): 117–22. http://dx.doi.org/10.1115/1.1842787.

Full text

Abstract:

In the present work the efficiency of the fluidized bed combustion (FBC) of high-volatile fuels and the extent of volatile matter post-combustion in the splashing zone and freeboard are investigated. A typical Mediterranean biomass (pine-seed shells) has been burned in a pilot-scale bubbling FB combustor (200 kWt) at different operating conditions. Both over-and under-bed fuel feeding options have been considered. A FBC model specifically developed for high-volatile fuels has been also applied to provide a comparison with bed carbon loading, in-bed heat release and splashing region temperature

APA, Harvard, Vancouver, ISO, and other styles

7

Zheng, Min, Fan Shen, and Pei Luo. "Vibration Fatigue Analysis of the Structure under Thermal Loading." Advanced Materials Research 853 (December 2013): 559–64. http://dx.doi.org/10.4028/www.scientific.net/amr.853.559.

Full text

Abstract:

The fatigue problem of structures under concurrent thermal and vibration loading has not been thoroughly studied even though it is common in applications of aero-engine combustor liners. Here we attempt to explore such a problem using a simplified combustor liner model that is implemented by the commercial finite element software ANSYS Workbench. The modal parameters at various temperatures are calculated and the fatigue behavior under stochastic base excitation and thermal environment are analyzed. The results show that thermal loading not only has an effect on dynamic characteristics but als

APA, Harvard, Vancouver, ISO, and other styles

8

Smajević, Izet, and Kemal Hanjalić. "Aerovalved Pulse Combustor for Enhancing Efficiency and Sustainability of Fossil Energy Conversion." B&H Electrical Engineering 17, s1 (2023): 53–60. http://dx.doi.org/10.2478/bhee-2023-0018.

Full text

Abstract:

Abstract The paper actualizes earlier research in developing a pulse combustion technique for enhancing the efficacy of utility and industrial boilers and furnaces. Some unpublished results of the experimental investigation of self-sustained pulsating combustion of a gas fuel in an aerovalved pulse combustor (PC) are presented. Relationships have been established between all important design and operating parameters and the combustion characteristics. It was demonstrated that a well-designed pulse combustor can operate efficiently in a stable self-pumping regime in a wide range of operating co

APA, Harvard, Vancouver, ISO, and other styles

9

Eckerle, W. A., and T. J. Rosfjord. "Soot loading in a generic gas turbine combustor." Journal of Propulsion and Power 4, no. 1 (1988): 89–96. http://dx.doi.org/10.2514/3.23036.

Full text

APA, Harvard, Vancouver, ISO, and other styles

10

Sun, Guo, and Yuan Gui Sun. "Thermal-Structural Analysis of Ni-Based Alloy Panel with Active Cooling Thermal Protection System." Applied Mechanics and Materials 644-650 (September 2014): 4718–21. http://dx.doi.org/10.4028/www.scientific.net/amm.644-650.4718.

Full text

Abstract:

In hypersonic environments, the development of aircraft engine presents the mitigation of the extreme thermal environment inside the combustion chamber. This paper establishes the capabilities for combustor panel design. By given the key loading and boundary conditions of the panel structure, the thermal structural analysis determines temperatures and stresses and the optimization improves panel’s robustness subject to thermal mechanical loads. A parametric sweep analysis is carried and the results give the optimal value of the panel face thickness.

APA, Harvard, Vancouver, ISO, and other styles

More sources

Dissertations / Theses on the topic "Combustor loading"

1

Ane, Chen Fu, and 陳福安. "Laser Diagnostics and Combustion Mechanism Investigation of High Loading Burners." Thesis, 2000. http://ndltd.ncl.edu.tw/handle/69376123082395290833.

Full text

APA, Harvard, Vancouver, ISO, and other styles

2

Mackay, John Bruce. "An investigation into the use of a compressed air loading mechanism as a means of improving the efficiency of a four stroke spark ignition internal combustion engine." Thesis, 2012. http://hdl.handle.net/10539/11607.

Full text

Abstract:

Internal combustion (I.C.) engines typically exhibit a characteristic ef ciency pro le which varies with operating load and engine speed, and it is widely known that the operating ef ciency is poor under low loading conditions. The objective of this project is to investigate whether an energy storing and recover- ing process, involving compressing air and subsequently using it for propulsion, could be used to achieve better overall ef ciency. An engine so modi ed would operate in two alternate modes. When using fuel, the engine operates as close to maximum ef ciency as practicable, with t

APA, Harvard, Vancouver, ISO, and other styles

Books on the topic "Combustor loading"

1

Effect of Equivalence Ratio and G-Loading on In-Situ Measurements of Chemiluminescence in an Ultra Compact Combustor. Storming Media, 2004.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

Book chapters on the topic "Combustor loading"

1

Kumawat, Sunil Kumar, Apurv Dilip Ghugare, Abhijeet Kumar, Srikrishna Sahu, and Ravikrishnan Vinu. "Nanoboron Slurry Fuel Droplet Combustion for High-Particle Loading Ratio." In Proceedings of the National Aerospace Propulsion Conference. Springer Nature Singapore, 2022. http://dx.doi.org/10.1007/978-981-19-2378-4_31.

Full text

APA, Harvard, Vancouver, ISO, and other styles

2

Gots, A. N. "Models of Fatigue Fracture Under Cyclic Loading Pistons of Internal Combustion Engines." In Proceedings of the 4th International Conference on Industrial Engineering. Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-95630-5_24.

Full text

APA, Harvard, Vancouver, ISO, and other styles

3

Li, Dayong, Yuling Shao, Zhenyu Qi, Minghao Zhang, Min Xia, and Xiaozhi Zhang. "Research Progress of Nano-combustion Catalyst Based on Graphene Loading Technology and Its Application." In Springer Proceedings in Physics. Springer Nature Singapore, 2022. http://dx.doi.org/10.1007/978-981-19-1774-5_15.

Full text

APA, Harvard, Vancouver, ISO, and other styles

4

Sadiki, Amsini, Mouldi Chrigui, Fernando Sacomano, and Assaad R. Masri. "Large Eddy Simulation of Diluted Turbulent Spray Combustion Based on FGM Methodology: Effect of fuel and Mass Loading." In Experiments and Numerical Simulations of Turbulent Combustion of Diluted Sprays. Springer International Publishing, 2014. http://dx.doi.org/10.1007/978-3-319-04678-5_5.

Full text

APA, Harvard, Vancouver, ISO, and other styles

5

Scala, Fabrizio, and Piero Salatino. "The Influence of Sorbent Properties and Reaction Conditions on Attrition of Limestone by Impact Loading in Fluidized Beds." In Proceedings of the 20th International Conference on Fluidized Bed Combustion. Springer Berlin Heidelberg, 2009. http://dx.doi.org/10.1007/978-3-642-02682-9_74.

Full text

APA, Harvard, Vancouver, ISO, and other styles

6

Barfusz, Oliver, Felix Hötte, Stefanie Reese, and Matthias Haupt. "Pseudo-transient 3D Conjugate Heat Transfer Simulation and Lifetime Prediction of a Rocket Combustion Chamber." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-53847-7_17.

Full text

Abstract:

Abstract Rocket engine nozzle structures typically fail after a few engine cycles due to the extreme thermomechanical loading near the nozzle throat. In order to obtain an accurate lifetime prediction and to increase the lifetime, a detailed understanding of the thermomechanical behavior and the acting loads is indispensable. The first part is devoted to a thermally coupled simulation (conjugate heat transfer) of a fatigue experiment. The simulation contains a thermal FEM model of the fatigue specimen structure, RANS simulations of nine cooling channel flows and a Flamelet-based RANS simulation of the hot gas flow. A pseudo-transient, implicit Dirichlet–Neumann scheme is utilized for the partitioned coupling. A comparison with the experiment shows a good agreement between the nodal temperatures and their corresponding thermocouple measurements. The second part consists of the lifetime prediction of the fatigue experiment utilizing a sequentially coupled thermomechanical analysis scheme. First, a transient thermal analysis is carried out to obtain the temperature field within the fatigue specimen. Afterwards, the computed temperature serves as input for a series of quasi-static mechanical analyses, in which a viscoplastic damage model is utilized. The evolution and progression of the damage variable within the regions of interest are thoroughly discussed. A comparison between simulation and experiment shows that the results are in good agreement. The crucial failure mode (doghouse effect) is captured very well.

APA, Harvard, Vancouver, ISO, and other styles

7

Das, Mithun. "Effect of Different Surface Types of Loading Vessel Wall on Combustion Performance of a Domestic LPG Cook Stove." In Advances in Thermal Engineering, Manufacturing, and Production Management. Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-16-2347-9_7.

Full text

APA, Harvard, Vancouver, ISO, and other styles

8

Okazaki, Masakazu, Satoshi Yamagishi, Motoki Sakaguchi, and Subramanian Rajivgandhi. "Specific Failures of Superalloys with Thermal Barrier Coatings Subjected to Thermo-Mechanical Fatigue Loadings with a Thermal Gradient in a Simulated Combustion Environment." In Superalloys 2012. John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118516430.ch49.

Full text

APA, Harvard, Vancouver, ISO, and other styles

9

Dunne, Fionn, and Nik Petrinic. "Creep in an aero-engine combustor material." In Introduction to Computational Plasticity. Oxford University PressOxford, 2005. http://dx.doi.org/10.1093/oso/9780198568261.003.0009.

Full text

Abstract:

Abstract Aero-engine components operating under in-service conditions are often subjected to a range of complex cyclic mechanical and thermal loading, leading to combined creep and cyclic plasticity. The polycrystalline nickel-base superalloy (C263) is a commercial alloy used for stationary components in aero-engines such as combustion chambers, casings, liners, exhaust ducting, and bearing housings. It is a fine-precipitate strengthened alloy at 800°C, with a precipitate solvus temperature of 925°C (Betteridge and Heslop, 1974). Combustion chamber applications require the material to undergo temperature fliuctuations between 20°C and 950°C, and the temperature range is therefore such that the precipitate solvus can be exceeded during in-service operation. significant microstructural change is therefore likely to occur during ordinary operation, leading to quite profound changes in the creep mechanisms in the material, controlling both deformation and component life.

APA, Harvard, Vancouver, ISO, and other styles

10

Campbell-Lochrie, Zakary, Carlos Walker-Ravena, Michael Gallagher, Nicholas Skowronski, Eric V. Mueller, and Rory M. Hadden. "Effect of Fuel Bed Structure on the Controlling Heat Transfer Mechanisms in Quiescent Porous Flame Spread." In Advances in Forest Fire Research 2022. Imprensa da Universidade de Coimbra, 2022. http://dx.doi.org/10.14195/978-989-26-2298-9_219.

Full text

Abstract:

The increasing importance of prescribed fire use has led to an increased focus on the development of modelling tools suited to conditions typical of prescribed fire scenarios. An improved understanding of flame spread through porous surface fuels represents an important part of these efforts. In the lower wind speed conditions typical of many prescribed burns, the role of fuel structure may be of greater importance than in highly wind-aided flame spread scenarios. The porous nature of wildland fuel beds complicates efforts to apply existing, solid surface theories for flame spread in low or quiescent wind conditions as radiation, convection and conduction may all occur within the porous fuel in addition to flame heating. An important first step in the development of any flame spread theory is the identification of the dominant heat transfer mechanisms but for wildland fuels the effect of fuel structure on the relative importance of different heating mechanisms must be considered. To investigate the role of fuel structure we therefore present a series of laboratory-based flame spread experiments conducted in pine needle fuel beds with various structural properties. The fuel loading and bulk density were independently varied by controlling the fuel bed height with water-cooled heat flux gauges used to measure the (radiant and total) heat flux from both the above-bed flame and the in-bed combustion region. A single dimensionless parameter (Î±ÏƒÎ´), incorporating the fuel bed porosity (Î±), fuel element surface-to-volume ratio (Ïƒ), and fuel bed height (Î´), was used to describe the overall fuel bed structure. The heat flux measurements highlighted the dominant role of in-bed heating across all of the studied fuel conditions although the magnitude of above-bed flame heating increased with increasing fuel loading. Heat fluxes from the in-bed combustion region exceeded those from the above-bed flame region with the magnitude of the peak (radiant and total) heat flux at each measurement location generally increasing with increasing Î±ÏƒÎ´ across the studied range (Î±ÏƒÎ´=49 to 399). However, the effect of fuel loading was also apparent with a positive relationship also observed between fuel loading and flame height. The experimentally observed effective heating distances also varied with bulk density and fuel loading and were used to evaluate the use of a thermal modelling approach incorporating the bulk structural properties of the porous fuel bed. Comparison with experimental observations of spread rate indicated a maximum variation in predicted spread rate of 29 % where only radiative transfer from the in-bed combustion region was considered, with closer agreement at lower Î±ÏƒÎ´ values. Where the contributions of both the in-bed and above-bed heat transfer mechanisms were considered, the need to incorporate additional heat loss terms into this thermal model were apparent. This study therefore emphasises the important role of porous fuel structure on the in-bed heat transfer and assesses suitable, physically meaningful structural descriptors. The experiments presented in this study will also provide a valuable dataset for future model development efforts incorporating measurements of fire behaviour and underlying physical phenomena across a wide range of structural conditions.

APA, Harvard, Vancouver, ISO, and other styles

Conference papers on the topic "Combustor loading"

1

Mestre, André, and Anne Cadiou. "Design and Experimentation of a Combustor for High Combustion Intensity." In ASME 1985 International Gas Turbine Conference and Exhibit. American Society of Mechanical Engineers, 1985. http://dx.doi.org/10.1115/85-gt-51.

Full text

Abstract:

The length and volume requirements of small gas turbines for missiles or propelled targets lead to combustor designs with high combustion intensity and large value of the air loading parameter Ω. The conventional combustors have used conditions corresponding to Ω values in the 1 to 10 kg m−3s−1 range. The increase of Ω required for combustors in missiles conduces for existing liners to a decrease of combustion efficiency and to an increase of pressure losses. Technical solutions have been worked out to make a combustor operating with a large air loading parameter: 25kgm-3s-1⩽Ω⩽50kgm-3s-1 and a

APA, Harvard, Vancouver, ISO, and other styles

2

Rosfjord, T. J. "Staged Combustor Evaluation of Low Rank Coal Fuels." In ASME 1988 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1988. http://dx.doi.org/10.1115/88-gt-91.

Full text

Abstract:

The combustion characteristics of fuels derived from low rank, coals have been evaluated at firing conditions representative of an industrial gas turbine engine. Data have been acquired for five fuels containing sub-bituminous coal and one using a lignite. The sub-bituminous fuels were coal-water mixtures differing in either the coal processing or coal loading. One slurry was based on minimally-processed coal which contained relatively high ash and internal moisture levels; the coal loading was limited to 42 pct to sustain acceptable handling. The other four slurries presented different loadin

APA, Harvard, Vancouver, ISO, and other styles

3

Zelina, J., and D. R. Ballal. "Combustor Stability and Emissions Research Using a Well Stirred Reactor." In ASME 1995 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1995. http://dx.doi.org/10.1115/95-gt-109.

Full text

Abstract:

The design and development of low-emissions, lean premixed aero or industrial gas turbine combustors is very challenging because it entails many compromises. To satisfy the projected CO and NOx emissions regulations without relaxing the conflicting requirements of combustion stability, efficiency, pattern factor, relight (for aero combustor) or off-peak loading (for industrial combustor) capability demands great design ingenuity. The well stirred reactor (WSR) provides a laboratory idealization of an efficient and highly compact advanced combustion system of the future that is capable of yield

APA, Harvard, Vancouver, ISO, and other styles

4

YONEZAWA, Y., H. TOH, S. GOTO, and M. OBATA. "Development of the jet-swirl high loading combustor." In 26th Joint Propulsion Conference. American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-2451.

Full text

APA, Harvard, Vancouver, ISO, and other styles

5

ECKERLE, W., and T. ROSFJORD. "Soot loading in a generic gas turbine combustor." In 25th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, 1987. http://dx.doi.org/10.2514/6.1987-297.

Full text

APA, Harvard, Vancouver, ISO, and other styles

6

Sasaki, Masafumi, Hirotaka Kumakura, and Daishi Suzuki. "Low NOx Combustor for Automotive Ceramic Gas Turbine: Conceptual Design." In ASME 1991 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1991. http://dx.doi.org/10.1115/91-gt-369.

Full text

Abstract:

Three low NOx combustors, i.e. a lean premixing combustor, a rich-lean two stage combustor and a lean diffusion flame combustor, were tested in order to find out a suitable combustion concept for an automotive ceramic gas turbine combustor. The prevaporization-premixing lean combustion was proposed as the most promising candidate to meet Japanese 10 mode regulation for gasoline passenger car. The required conditions for the uniform premixture formation in the prevaporization-premixing tube were achieved by a fine droplet size atomizer and by means of swirl and turbulent generator. Air ratio ra

APA, Harvard, Vancouver, ISO, and other styles

7

Cronemyr, Peter J. M., Chris J. Hulme, and Christian Troger. "Coupled Acoustic-Structure Analysis of an Annular DLE Combustor." In ASME 1998 International Gas Turbine and Aeroengine Congress and Exhibition. American Society of Mechanical Engineers, 1998. http://dx.doi.org/10.1115/98-gt-502.

Full text

Abstract:

With the advent of today’s dry low emission (DLE) combustors for industrial gas turbines (GT), an additional type of load case other than thermal loading on the combustor structure, has put itself heavily into focus, namely pulsation loading. Although recognised for decades in rocket engines and ram-jets, it was not until the incorporation of diluted flames and completely closed combustors, used to reduce NOx emissions, that thermo-acoustically excited pressure pulsations became an issue in the design of industrial GT combustors. This paper presents the computational methods that are available

APA, Harvard, Vancouver, ISO, and other styles

8

BUTLER, G. "Coalescence/dispersion modeling of non-steady high intensity combustor loading." In 21st Joint Propulsion Conference. American Institute of Aeronautics and Astronautics, 1985. http://dx.doi.org/10.2514/6.1985-1442.

Full text

APA, Harvard, Vancouver, ISO, and other styles

9

Bohan, Brian T., and Marc D. Polanka. "A New Spin on Small-Scale Combustor Geometry." In ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2018. http://dx.doi.org/10.1115/gt2018-75338.

Full text

Abstract:

The Ultra Compact Combustor (UCC) is an innovative combustor system alternative to traditional turbine engine combustors with the potential for engine efficiency improvements with a reduced volume. Historically, the UCC cavity had been configured such that highly centrifugally loaded combustion took place in a recessed circumferential cavity positioned around the outside diameter of the engine. One of the obstacles with this design was that the combustion products had to migrate radially across the span of a vane while being pushed downstream by a central core flow. This configuration proved d

APA, Harvard, Vancouver, ISO, and other styles

10

Belokon, Alexandr A., Konstantin M. Khritov, Lev A. Klyachko, Sergey A. Tschepin, Vladimir M. Zakharov, and George Opdyke. "Prediction of Combustion Efficiency and NOx Levels for Diffusion Flame Combustors in HAT Cycles." In ASME Turbo Expo 2002: Power for Land, Sea, and Air. ASMEDC, 2002. http://dx.doi.org/10.1115/gt2002-30609.

Full text

Abstract:

Diffusion flame combustor test results are presented for methane firing in steam/air mixtures containing up to 20% steam. The tests were conducted at atmospheric pressure with combustor inlet temperatures up to 700K. Steam and air were fully premixed before combustion. Combustion efficiency and NOX levels were measured. The well-known Θ loading parameter was modified by replacing the combustor inlet temperature with the flame temperature. The flame temperature was defined as the stoichiometric temperature of the steam/air mixture. The combustion efficiency obtained with and without steam corre

APA, Harvard, Vancouver, ISO, and other styles

Reports on the topic "Combustor loading"

1

Greenhalgh, W. O. Combustion and fuel loading characteristics of Hanford Site transuranic solid waste. Office of Scientific and Technical Information (OSTI), 1994. http://dx.doi.org/10.2172/10180206.

Full text

APA, Harvard, Vancouver, ISO, and other styles

2

Kuo, Kenneth K., and Pete Ferrara. Flame Spreading and Combustion Behavior of Gun Propellants Packed in High Loading Densities. Defense Technical Information Center, 2004. http://dx.doi.org/10.21236/ada426407.

Full text

APA, Harvard, Vancouver, ISO, and other styles

3

Price, Matthew A. Effects of Cylindrical Charge Geometry and Secondary Combustion Reactions on the Internal Blast Loading of Reinforced Concrete Structures. Office of Scientific and Technical Information (OSTI), 2005. http://dx.doi.org/10.2172/841586.

Full text

APA, Harvard, Vancouver, ISO, and other styles

4

Norfleet, Quickel, and Beavers. PR-186-12204-R02 Guidelines on the Effects of Ethanol on Pump Stations and Terminal Facilities. Pipeline Research Council International, Inc. (PRCI), 2013. http://dx.doi.org/10.55274/r0010673.

Full text

Abstract:

Ethanol has been used for the last several years as an environmentally friendly alternative to methyl tertbutyl ether (MTBE), which is an oxygenate additive to gasoline, to increase octane levels, and to facilitate the combustion process. However, the need to find alternatives to imported oil and gas has spurred the increased use of ethanol as an alternative fuel source. Further, ethanol is being promoted as a potential trade-off for CO2 emissions from the burning of fossil fuels since CO2 is consumed by the plants used as the ethanol source. Legislation mandates a significant increase in etha

APA, Harvard, Vancouver, ISO, and other styles

We offer discounts on all premium plans for authors whose works are included in thematic literature selections. Contact us to get a unique promo code!