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Статті в журналах з теми "Aeronautical turbine"
Sarti Leme, Alexandre Domingos, Geraldo Creci, Edilson Rosa Barbosa de Jesus, Túlio César Rodrigues, and 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 (April 2019): 15–26. http://dx.doi.org/10.4028/www.scientific.net/aef.32.15.
Повний текст джерелаZhang, Bing, Jian-Guo Gao, Gui-Long Min, and 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.
Повний текст джерелаDunham, J. "50 years of turbomachinery research at Pyestock — part 2: turbines." Aeronautical Journal 104, no. 1034 (April 2000): 199–207. http://dx.doi.org/10.1017/s0001924000028104.
Повний текст джерелаDediu, Gabriel, and Daniel Eugeniu Crunteanu. "Automatic Control System for Gas Turbines Test Rig." Applied Mechanics and Materials 436 (October 2013): 398–405. http://dx.doi.org/10.4028/www.scientific.net/amm.436.398.
Повний текст джерелаLemco, Ian. "Wittgenstein's aeronautical investigation." Notes and Records of the Royal Society 61, no. 1 (December 22, 2006): 39–51. http://dx.doi.org/10.1098/rsnr.2006.0163.
Повний текст джерелаDunham, J. "50 years of turbomachinery research at Pyestock — part one: compressors." Aeronautical Journal 104, no. 1033 (March 2000): 141–51. http://dx.doi.org/10.1017/s0001924000025331.
Повний текст джерелаSaenz-Aguirre, Aitor, Sergio Fernandez-Resines, Iñigo Aramendia, Unai Fernandez-Gamiz, Ekaitz Zulueta, Jose Manuel Lopez-Guede, and Javier Sancho. "5 MW Wind Turbine Annual Energy Production Improvement by Flow Control Devices." Proceedings 2, no. 23 (November 6, 2018): 1452. http://dx.doi.org/10.3390/proceedings2231452.
Повний текст джерелаBassi, Stefano, Matteo Scafe, Enrico Leoni, Claudio Mingazzini, Narayan Jatinder Bhatia, and 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.
Повний текст джерелаFatsis, Antonios. "Performance Enhancement of One and Two-Shaft Industrial Turboshaft Engines Topped With Wave Rotors." International Journal of Turbo & Jet-Engines 35, no. 2 (May 25, 2018): 137–47. http://dx.doi.org/10.1515/tjj-2016-0040.
Повний текст джерелаBrookes, Stephen Peter, Hans Joachim Kühn, Birgit Skrotzki, Hellmuth Klingelhöffer, Rainer Sievert, Janine Pfetzing, Dennis Peter, and Gunther F. Eggeler. "Multi-Axial Thermo-Mechanical Fatigue of a Near-Gamma TiAl-Alloy." Advanced Materials Research 59 (December 2008): 283–87. http://dx.doi.org/10.4028/www.scientific.net/amr.59.283.
Повний текст джерелаДисертації з теми "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.
Повний текст джерелаAl-Khudairi, Othman. "Structural performance of horizontal axis wind turbine blade." Thesis, Kingston University, 2014. http://eprints.kingston.ac.uk/32197/.
Повний текст джерелаDupuy, Fabien. "Reduced Order Models and Large Eddy Simulation for Combustion Instabilities in aeronautical Gas Turbines." Thesis, Toulouse, INPT, 2020. http://www.theses.fr/2020INPT0046.
Повний текст джерелаIncreasingly 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.
Повний текст джерелаSharma 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/.
Повний текст джерелаOksuz, 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.
Повний текст джерелаAkagi, Raymond. "Ram Air-Turbine of Minimum Drag." DigitalCommons@CalPoly, 2021. https://digitalcommons.calpoly.edu/theses/2261.
Повний текст джерелаNotarianni, 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.
Знайти повний текст джерелаGorgulu, 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.
Повний текст джерелаmodel, 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/.
Повний текст джерелаКниги з теми "Aeronautical turbine"
Rogo, C. Variable area radial turbine fabrication and test program. [Cleveland, Ohio: Army Aviation Research & Technology Activity, Propulsion Directorate, 1986.
Знайти повний текст джерелаBill, Gunston. The development of jet and turbine aero engines. Yeovil: Patrick Stephens, 1995.
Знайти повний текст джерелаCenter), 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.
Знайти повний текст джерелаAerothermodynamics of gas turbine and rocket propulsion. 3rd ed. Reston, VA: American Institute of Aeronautics and Astronautics, 1997.
Знайти повний текст джерелаAerothermodynamics of gas turbine and rocket propulsion. Washington, DC: American Institute of Aeronautics and Astronautics, 1988.
Знайти повний текст джерелаL, Braslow Albert, Butterfield A. J, and Langley Research Center, eds. Circulation control propellers for general aviation, including a BASIC computer program. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.
Знайти повний текст джерела1959-, Pierre Christophe, and United States. National Aeronautics and Space Administration., eds. Stochastic sensitivity measure for mistuned high-performance turbines. [Washington, DC]: National Aeronautics and Space Administration, 1992.
Знайти повний текст джерелаJ, Holt Mark, ed. The turbine pilot's flight manual. Ames: Iowa State University Press, 1995.
Знайти повний текст джерелаJ, Holt Mark, ed. The turbine pilot's flight manual. 2nd ed. Ames: Iowa State University Press, 2001.
Знайти повний текст джерелаC, 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.
Знайти повний текст джерелаЧастини книг з теми "Aeronautical turbine"
Xu, You Liang, Cheng Li Liu, and Zhen Zhou Lu. "Fuzzy-Random FOSM and its Application in Low Cycle Fatigue Life Reliability Analysis of an Aeronautical Engine Turbine Disk." In Fracture and Damage Mechanics V, 775–78. Stafa: Trans Tech Publications Ltd., 2006. http://dx.doi.org/10.4028/0-87849-413-8.775.
Повний текст джерелаVinogradov, K., and G. Kretinin. "Application of UQ for Turbine Blade CHT Computations." In 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.
Повний текст джерела"Engine MDO Deployed on a Two-Stage Turbine." In 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.
Повний текст джерелаAzevedo, Jéssica Fernanda de, Viviane Teleginski Mazur, Daniele Cristina Chagas, Júlio César Gomes Santos, Maurício Marlon Mazur, and Getúlio de Vasconcelos. "THICKNESS CONTROL OF COATINGS DEPOSITED BY CO2 LASER FOR AERONAUTICAL TURBINE BLADES." In Engenharia Mecânica: Inovações Tecnológicas de Elevado Valor, 1–7. Atena Editora, 2021. http://dx.doi.org/10.22533/at.ed.8262109021.
Повний текст джерелаTudosie, Alexandru-Nicolae. "Aircraft Gas-Turbine Engine’s Control Based on the Fuel Injection Control." In Aeronautics and Astronautics. InTech, 2011. http://dx.doi.org/10.5772/17986.
Повний текст джерелаKollmann, Karl, Calum E. Douglas, and S. Can Gülen. "Prelude." In 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.
Повний текст джерелаТези доповідей конференцій з теми "Aeronautical turbine"
Rouser, Kurt P., Caitlin R. Thorn, Aaron R. Byerley, Charles F. Wisniewski, Scott R. Nowlin, and Kenneth W. Van Treuren. "Integration of a Turbine Cascade Facility Into an Undergraduate Thermo-Propulsion Sequence." In ASME Turbo Expo 2013: Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/gt2013-94744.
Повний текст джерелаTomita, Jesuino Takachi, João Roberto Barbosa, and Cleverson Bringhenti. "The Flow Machines Course at the Technological Institute of Aeronautics for Mechanical-Aeronautical Engineering Undergraduate Course." In ASME Turbo Expo 2013: Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/gt2013-95228.
Повний текст джерелаSilva, Elizabete, and Reyolando Brasil. "Localization of vibration modes in aeronautical turbine blades." In 8th International Symposium on Solid Mechanics. ABCM, 2022. http://dx.doi.org/10.26678/abcm.mecsol2022.msl22-0129.
Повний текст джерелаAndriani, Roberto, Fausto Gamma, and Umberto Ghezzi. "Main Effects of Intercooling and Regeneration on Aeronautical Gas Turbine Engines." In 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.
Повний текст джерелаCirtwill, Joseph D., Sina Kheirkhah, Pankaj Saini, Krishna Venkatesan, and Adam M. Steinberg. "Analysis of intermittent thermoacoustic oscillations in an aeronautical gas turbine combustor." In 55th AIAA Aerospace Sciences Meeting. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2017. http://dx.doi.org/10.2514/6.2017-0824.
Повний текст джерелаMotheau, Emmanuel, Franck Nicoud, Yoann Mery, and Thierry Poinsot. "Analysis and Modelling of Entropy Modes in a Realistic Aeronautical Gas Turbine." In ASME Turbo Expo 2013: Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/gt2013-94224.
Повний текст джерелаMa, Zhiwen, Comas Haynes, and Pinakin Patel. "System Level Synthesis, Modeling and Roadmapping for Aeronautical SOFC/Gas Turbine Hybrid Systems." In ASME 2005 International Mechanical Engineering Congress and Exposition. ASMEDC, 2005. http://dx.doi.org/10.1115/imece2005-80055.
Повний текст джерелаRolling, August J., Aaron R. Byerley, and Charles F. Wisniewski. "Integrating Systems Engineering Into the USAF Academy Capstone Gas Turbine Engine Course." In ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition. ASMEDC, 2011. http://dx.doi.org/10.1115/gt2011-46440.
Повний текст джерелаGiusti, Andrea, Luca Magri, and Marco Zedda. "Flow Inhomogeneities in a Realistic Aeronautical Gas-Turbine Combustor: Formation, Evolution and Indirect Noise." In ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2018. http://dx.doi.org/10.1115/gt2018-76436.
Повний текст джерелаByerley, Aaron R., August J. Rolling, and Kenneth W. Van Treuren. "Estimating Gas Turbine Engine Weight, Costs, and Development Time During the Preliminary Aircraft Engine Design Process." In ASME Turbo Expo 2013: Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/gt2013-95778.
Повний текст джерела