Littérature scientifique sur le sujet « Aeronautical turbine »
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Articles de revues sur le sujet "Aeronautical turbine"
Sarti Leme, Alexandre Domingos, Geraldo Creci, Edilson Rosa Barbosa de Jesus, Túlio César Rodrigues et João Carlos Menezes. « Finite Element Analysis to Verify the Structural Integrity of an Aeronautical Gas Turbine Disc Made from Inconel 713LC Superalloy ». Advanced Engineering Forum 32 (avril 2019) : 15–26. http://dx.doi.org/10.4028/www.scientific.net/aef.32.15.
Texte intégralZhang, Bing, Jian-Guo Gao, Gui-Long Min et Shoushuo Liu. « Reliability analysis of gear transmission system of aeronautical turbine starter under multi-constraint ». Thermal Science 24, no 3 Part A (2020) : 1513–20. http://dx.doi.org/10.2298/tsci190517016z.
Texte intégralDunham, J. « 50 years of turbomachinery research at Pyestock — part 2 : turbines ». Aeronautical Journal 104, no 1034 (avril 2000) : 199–207. http://dx.doi.org/10.1017/s0001924000028104.
Texte intégralDediu, Gabriel, et Daniel Eugeniu Crunteanu. « Automatic Control System for Gas Turbines Test Rig ». Applied Mechanics and Materials 436 (octobre 2013) : 398–405. http://dx.doi.org/10.4028/www.scientific.net/amm.436.398.
Texte intégralLemco, Ian. « Wittgenstein's aeronautical investigation ». Notes and Records of the Royal Society 61, no 1 (22 décembre 2006) : 39–51. http://dx.doi.org/10.1098/rsnr.2006.0163.
Texte intégralDunham, J. « 50 years of turbomachinery research at Pyestock — part one : compressors ». Aeronautical Journal 104, no 1033 (mars 2000) : 141–51. http://dx.doi.org/10.1017/s0001924000025331.
Texte intégralSaenz-Aguirre, Aitor, Sergio Fernandez-Resines, Iñigo Aramendia, Unai Fernandez-Gamiz, Ekaitz Zulueta, Jose Manuel Lopez-Guede et Javier Sancho. « 5 MW Wind Turbine Annual Energy Production Improvement by Flow Control Devices ». Proceedings 2, no 23 (6 novembre 2018) : 1452. http://dx.doi.org/10.3390/proceedings2231452.
Texte intégralBassi, Stefano, Matteo Scafe, Enrico Leoni, Claudio Mingazzini, Narayan Jatinder Bhatia et Andrea Rossi. « Development of recyclable Fibre Metal Laminates (FML), their mechanical characterization and FE modelling, aiming at structural application in aeronautics ». MATEC Web of Conferences 349 (2021) : 01010. http://dx.doi.org/10.1051/matecconf/202134901010.
Texte intégralFatsis, Antonios. « Performance Enhancement of One and Two-Shaft Industrial Turboshaft Engines Topped With Wave Rotors ». International Journal of Turbo & ; Jet-Engines 35, no 2 (25 mai 2018) : 137–47. http://dx.doi.org/10.1515/tjj-2016-0040.
Texte intégralBrookes, Stephen Peter, Hans Joachim Kühn, Birgit Skrotzki, Hellmuth Klingelhöffer, Rainer Sievert, Janine Pfetzing, Dennis Peter et Gunther F. Eggeler. « Multi-Axial Thermo-Mechanical Fatigue of a Near-Gamma TiAl-Alloy ». Advanced Materials Research 59 (décembre 2008) : 283–87. http://dx.doi.org/10.4028/www.scientific.net/amr.59.283.
Texte intégralThèses sur le sujet "Aeronautical turbine"
Koupper, Charlie. « Unsteady multi-component simulations dedicated to the impact of the combustion chamber on the turbine of aeronautical gas turbines ». Phd thesis, Toulouse, INPT, 2015. http://oatao.univ-toulouse.fr/14187/1/koupper_partie_1_sur_2.pdf.
Texte intégralAl-Khudairi, Othman. « Structural performance of horizontal axis wind turbine blade ». Thesis, Kingston University, 2014. http://eprints.kingston.ac.uk/32197/.
Texte intégralDupuy, Fabien. « Reduced Order Models and Large Eddy Simulation for Combustion Instabilities in aeronautical Gas Turbines ». Thesis, Toulouse, INPT, 2020. http://www.theses.fr/2020INPT0046.
Texte intégralIncreasingly stringent regulations as well as environmental concerns have lead gas turbine powered engine manufacturers to develop the current generation of combustors, which feature lower than ever fuel consumption and pollutant emissions. However, modern combustor designs have been shown to be prone to combustion instabilities, where the coupling between acoustics of the combustor and the flame results in large pressure oscillations and vibrations within the combustion chamber. These instabilities can cause structural damages to the engine or even lead to its destruction. At the same time, considerable developments have been achieved in the numerical simulation domain, and Computational Fluid Dynamics (CFD) has proven capable of capturing unsteady flame dynamics and combustion instabilities for aforementioned engines. Still, even with the current large and fast increasing computing capabilities, time remains the key constraint for these high fidelity yet computationally intensive calculations. Typically, covering the entire range of operating conditions for an industrial engine is still out of reach. In that respect, low order models exist and can be efficient at predicting the occurrence of combustion instabilities, provided an adequate modeling of the flame/acoustics interaction as appearing in the system is available. This essential piece of information is usually recast as the so called Flame Transfer Function (FTF) relating heat release rate fluctuations to velocity fluctuations at a given point. One way to obtain this transfer function is to rely on analytical models, but few exist for turbulent swirling flames. Another way consists in performing costly experiments or numerical simulations, negating the requested fast prediction capabilities. This thesis therefore aims at providing fast, yet reliable methods to allow for low order combustion instabilities modeling. In that context, understanding the underlying mechanisms of swirling flame acoustic response is also targeted. To address this issue, a novel hybrid approach is first proposed based on a reduced set of high fidelity simulations that can be used to determine input parameters of an analytical model used to express the FTF of premixed swirling flames. The analytical model builds on previous works starting with a level-set description of the flame front dynamics while also accounting for the acoustic-vorticity conversion through a swirler. For such a model, validation is obtained using reacting stationary and pulsed numerical simulations of a laboratory scale premixed swirl stabilized flame. The model is also shown to be able to handle various perturbation amplitudes. At last, 3D high fidelity simulations of an industrial gas turbine powered by a swirled spray flame are performed to determine whether a combustion instability observed in experiments can be predicted using numerical analysis. To do so, a series of forced simulations is carried out in en effort to highlight the importance of the two-phase flow flame response evaluation. In that case, sensitivity to reference velocity perturbation probing positions as well as the amplitude and location of the acoustic perturbation source are investigated. The analytical FTF model derived in the context of a laboratory premixed swirled burner is furthermore gauged in this complex case. Results show that the unstable mode is predicted by the acoustic analysis, but that the flame model proposed needs further improvements to extend its applicability range and thus provide data relevant to actual aero-engines
Elfarra, Monier A. K. « Horizontal Axis Wind Turbine Rotor Blade : Winglet And Twist Aerodynamic Design And Optimization Using Cfd ». Phd thesis, METU, 2011. http://etd.lib.metu.edu.tr/upload/12612987/index.pdf.
Texte intégralSharma has shown the best agreement with measurements. Launder &ndash
Sharma was chosen for further simulations and for the design process. Before starting the design and optimization, different winglet configurations were studied. The winglets pointing towards the suction side of the blade have yielded higher power output. Genetic algorithm and artificial neural network were implemented in the design and optimization process. The optimized winglet has shown an increase in power of about 9.5 % where the optimized twist has yielded to an increase of 4%. Then the stall regulated blade has been converted into pitch regulated blade to yield more power output. The final design was produced by a combination of the optimized winglet, optimized twist andbest pitch angle for every wind speed. The final design has shown an increase in power output of about 38%.
Effendy, Marwan. « Investigation of turbine blade trailing edge cooling and thermal mixing characteristics ». Thesis, Kingston University, 2014. http://eprints.kingston.ac.uk/30604/.
Texte intégralOksuz, Ozhan. « Multiploid Genetic Algorithms For Multi-objective Turbine Blade Aerodynamic Optimization ». Phd thesis, METU, 2007. http://etd.lib.metu.edu.tr/upload/12609196/index.pdf.
Texte intégralAkagi, Raymond. « Ram Air-Turbine of Minimum Drag ». DigitalCommons@CalPoly, 2021. https://digitalcommons.calpoly.edu/theses/2261.
Texte intégralNotarianni, Gianmarco. « Analysis and modelling of the turbocharger behavior of an internal combustion engine for aeronautical application ». Master's thesis, Alma Mater Studiorum - Università di Bologna, 2019.
Trouver le texte intégralGorgulu, Ilhan. « Numerical Simulation Of Turbine Internal Cooling And Conjugate Heat Transfer Problems With Rans-based Turbulance Models ». Master's thesis, METU, 2012. http://etd.lib.metu.edu.tr/upload/12615000/index.pdf.
Texte intégralmodel, Shear Stress Transport k-&omega
model, Reynolds Stress Model and V2-f model, which became increasingly popular during the last few years, have been used at the numerical simulations. According to conducted analyses, despite a few unreasonable predictions, in the majority of the numerical simulations, V2-f model outperforms other first-order turbulence models (Realizable k-&epsilon
and Shear Stress Transport k-&omega
) in terms of accuracy and Reynolds Stress Model in terms of convergence.
Boiani, Davide. « Finite element structural and thermal analysis of JT9D turbofan engine first stage turbine blade ». Bachelor's thesis, Alma Mater Studiorum - Università di Bologna, 2017. http://amslaurea.unibo.it/12566/.
Texte intégralLivres sur le sujet "Aeronautical turbine"
Rogo, C. Variable area radial turbine fabrication and test program. [Cleveland, Ohio : Army Aviation Research & Technology Activity, Propulsion Directorate, 1986.
Trouver le texte intégralBill, Gunston. The development of jet and turbine aero engines. Yeovil : Patrick Stephens, 1995.
Trouver le texte intégralCenter), NASA-Chinese Aeronautical Establishment (CAE) Symposium (1985 NASA Lewis Research. Combustion fundamentals : NASA-Chinese Aeronautical Establishment (CAE) Symposium. [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
Trouver le texte intégralAerothermodynamics of gas turbine and rocket propulsion. 3e éd. Reston, VA : American Institute of Aeronautics and Astronautics, 1997.
Trouver le texte intégralAerothermodynamics of gas turbine and rocket propulsion. Washington, DC : American Institute of Aeronautics and Astronautics, 1988.
Trouver le texte intégralL, Braslow Albert, Butterfield A. J et Langley Research Center, dir. Circulation control propellers for general aviation, including a BASIC computer program. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1985.
Trouver le texte intégral1959-, Pierre Christophe, et United States. National Aeronautics and Space Administration., dir. Stochastic sensitivity measure for mistuned high-performance turbines. [Washington, DC] : National Aeronautics and Space Administration, 1992.
Trouver le texte intégralJ, Holt Mark, dir. The turbine pilot's flight manual. Ames : Iowa State University Press, 1995.
Trouver le texte intégralJ, Holt Mark, dir. The turbine pilot's flight manual. 2e éd. Ames : Iowa State University Press, 2001.
Trouver le texte intégralC, Smith Steven. Airflow calibration of a bellmouth inlet for measurement of compressor airflow in turbine-powered propulsion simulators. Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 1985.
Trouver le texte intégralChapitres de livres sur le sujet "Aeronautical turbine"
Xu, You Liang, Cheng Li Liu et Zhen Zhou Lu. « Fuzzy-Random FOSM and its Application in Low Cycle Fatigue Life Reliability Analysis of an Aeronautical Engine Turbine Disk ». Dans Fracture and Damage Mechanics V, 775–78. Stafa : Trans Tech Publications Ltd., 2006. http://dx.doi.org/10.4028/0-87849-413-8.775.
Texte intégralVinogradov, K., et G. Kretinin. « Application of UQ for Turbine Blade CHT Computations ». Dans Uncertainty Management for Robust Industrial Design in Aeronautics, 365–81. Cham : Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-77767-2_23.
Texte intégral« Engine MDO Deployed on a Two-Stage Turbine ». Dans Advances in Collaborative Civil Aeronautical Multidisciplinary Design Optimization, 289–330. Reston ,VA : American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/5.9781600867279.0289.0330.
Texte intégralAzevedo, Jéssica Fernanda de, Viviane Teleginski Mazur, Daniele Cristina Chagas, Júlio César Gomes Santos, Maurício Marlon Mazur et Getúlio de Vasconcelos. « THICKNESS CONTROL OF COATINGS DEPOSITED BY CO2 LASER FOR AERONAUTICAL TURBINE BLADES ». Dans Engenharia Mecânica : Inovações Tecnológicas de Elevado Valor, 1–7. Atena Editora, 2021. http://dx.doi.org/10.22533/at.ed.8262109021.
Texte intégralTudosie, Alexandru-Nicolae. « Aircraft Gas-Turbine Engine’s Control Based on the Fuel Injection Control ». Dans Aeronautics and Astronautics. InTech, 2011. http://dx.doi.org/10.5772/17986.
Texte intégralKollmann, Karl, Calum E. Douglas et S. Can Gülen. « Prelude ». Dans Turbo/Supercharger Compressors and Turbines for Aircraft Propulsion in WWII : Theory, History and Practice—Guidance from the Past for Modern Engineers and Students, 1–7. ASME, 2021. http://dx.doi.org/10.1115/1.884676_ch1.
Texte intégralActes de conférences sur le sujet "Aeronautical turbine"
Rouser, Kurt P., Caitlin R. Thorn, Aaron R. Byerley, Charles F. Wisniewski, Scott R. Nowlin et Kenneth W. Van Treuren. « Integration of a Turbine Cascade Facility Into an Undergraduate Thermo-Propulsion Sequence ». Dans ASME Turbo Expo 2013 : Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/gt2013-94744.
Texte intégralTomita, Jesuino Takachi, João Roberto Barbosa et Cleverson Bringhenti. « The Flow Machines Course at the Technological Institute of Aeronautics for Mechanical-Aeronautical Engineering Undergraduate Course ». Dans ASME Turbo Expo 2013 : Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/gt2013-95228.
Texte intégralSilva, Elizabete, et Reyolando Brasil. « Localization of vibration modes in aeronautical turbine blades ». Dans 8th International Symposium on Solid Mechanics. ABCM, 2022. http://dx.doi.org/10.26678/abcm.mecsol2022.msl22-0129.
Texte intégralAndriani, Roberto, Fausto Gamma et Umberto Ghezzi. « Main Effects of Intercooling and Regeneration on Aeronautical Gas Turbine Engines ». Dans 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Reston, Virigina : American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-6539.
Texte intégralCirtwill, Joseph D., Sina Kheirkhah, Pankaj Saini, Krishna Venkatesan et Adam M. Steinberg. « Analysis of intermittent thermoacoustic oscillations in an aeronautical gas turbine combustor ». Dans 55th AIAA Aerospace Sciences Meeting. Reston, Virginia : American Institute of Aeronautics and Astronautics, 2017. http://dx.doi.org/10.2514/6.2017-0824.
Texte intégralMotheau, Emmanuel, Franck Nicoud, Yoann Mery et Thierry Poinsot. « Analysis and Modelling of Entropy Modes in a Realistic Aeronautical Gas Turbine ». Dans ASME Turbo Expo 2013 : Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/gt2013-94224.
Texte intégralMa, Zhiwen, Comas Haynes et Pinakin Patel. « System Level Synthesis, Modeling and Roadmapping for Aeronautical SOFC/Gas Turbine Hybrid Systems ». Dans ASME 2005 International Mechanical Engineering Congress and Exposition. ASMEDC, 2005. http://dx.doi.org/10.1115/imece2005-80055.
Texte intégralRolling, August J., Aaron R. Byerley et Charles F. Wisniewski. « Integrating Systems Engineering Into the USAF Academy Capstone Gas Turbine Engine Course ». Dans ASME 2011 Turbo Expo : Turbine Technical Conference and Exposition. ASMEDC, 2011. http://dx.doi.org/10.1115/gt2011-46440.
Texte intégralGiusti, Andrea, Luca Magri et Marco Zedda. « Flow Inhomogeneities in a Realistic Aeronautical Gas-Turbine Combustor : Formation, Evolution and Indirect Noise ». Dans ASME Turbo Expo 2018 : Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2018. http://dx.doi.org/10.1115/gt2018-76436.
Texte intégralByerley, Aaron R., August J. Rolling et Kenneth W. Van Treuren. « Estimating Gas Turbine Engine Weight, Costs, and Development Time During the Preliminary Aircraft Engine Design Process ». Dans ASME Turbo Expo 2013 : Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/gt2013-95778.
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