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Artykuły w czasopismach na temat "Rotors"
Hou, Xukui, Ende Wang, Hui Cao, Yalong Zhu i Kai Qi. "Research on Dynamic Balance Adjustment Method of Single Braced Frame Gyroscope Rotor". MATEC Web of Conferences 256 (2019): 02005. http://dx.doi.org/10.1051/matecconf/201925602005.
Pełny tekst źródłaKay, Matthew W., Gregory P. Walcott, James D. Gladden, Sharon B. Melnick i Jack M. Rogers. "Lifetimes of epicardial rotors in panoramic optical maps of fibrillating swine ventricles". American Journal of Physiology-Heart and Circulatory Physiology 291, nr 4 (październik 2006): H1935—H1941. http://dx.doi.org/10.1152/ajpheart.00276.2006.
Pełny tekst źródłaPrasad Rao, Jubilee, Jonathan E. Holzsager, Marco M. Maia i Javier F. Diez. "Experimental Study into Optimal Configuration and Operation of Two-Four Rotor Coaxial Systems for eVTOL Vehicles". Aerospace 9, nr 8 (17.08.2022): 452. http://dx.doi.org/10.3390/aerospace9080452.
Pełny tekst źródłaLiu, Bao Guo, Hai Feng Hua, Long Wang Yue i Xiao Ding Xu. "Design of the Post-Processor for Rotors Dynamics Based on the STEP Standard". Advanced Materials Research 706-708 (czerwiec 2013): 1871–76. http://dx.doi.org/10.4028/www.scientific.net/amr.706-708.1871.
Pełny tekst źródłaAndrew, Philip L. "GE Power Services Ships First F-class Extended-Life Rotors". Mechanical Engineering 138, nr 05 (1.05.2016): 54–55. http://dx.doi.org/10.1115/1.2016-may-4.
Pełny tekst źródłaLaube, Tomasz, i Janusz Piechna. "Analytical and Numerical Feasibility Analysis of a Contra-Rotary Ramjet Engine". Energies 13, nr 1 (30.12.2019): 163. http://dx.doi.org/10.3390/en13010163.
Pełny tekst źródłaPervushin, Vladimir F. "Classification of rotary cultivation tools of agricultural machines and their motion trajectories". Agricultural Engineering, nr 3 (2023): 57–64. http://dx.doi.org/10.26897/2687-1149-2023-3-57-64.
Pełny tekst źródłaKong, Yong-Boon, J. V. R. Prasad, Lakshmi N. Sankar i Chengjian He. "Finite State Inflow Flow Model for Coaxial Rotor Configuration". Journal of the American Helicopter Society 65, nr 3 (1.07.2020): 1–11. http://dx.doi.org/10.4050/jahs.65.032002.
Pełny tekst źródłaMimmi, G., i P. Pennacchi. "Analytical model of a particular type of positive displacement blower". Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science 213, nr 5 (1.05.1999): 517–26. http://dx.doi.org/10.1243/0954406991522743.
Pełny tekst źródłaQian, Kun Xi, Z. H. Xu i H. Wang. "Effects of Rotational Inertia and Bearing Force on Stability of Permanent Maglev Rotator". Applied Mechanics and Materials 150 (styczeń 2012): 50–56. http://dx.doi.org/10.4028/www.scientific.net/amm.150.50.
Pełny tekst źródłaRozprawy doktorskie na temat "Rotors"
Guirao, Victor Suman [UNESP]. "Mancais magnéticos ativos para atenuação de vibrações em eixos rotativos". Universidade Estadual Paulista (UNESP), 2012. http://hdl.handle.net/11449/94526.
Pełny tekst źródłaCoordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)
Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)
Este trabalho trata do controle de vibrações em rotores utilizando mancais magnéticos ativos. Foram apresentadas simulações numéricas para o posicionamento ótimo de um atuador magnético utilizado para atenuar vibrações em rotor apoiado por mancais convencionais. O posicionamento ótimo do atuador foi implementado utilizando como função objetivo as normas H2 e H∞. Para modelar o rotor foi utilizado o método de elementos finitos (MEF) e a técnica de redução pseudo-modal para diminuir o esforço computacional durante o controle. As simulações mostraram que um bom posicionamento do atuador aliado ao controle LQR proporcionam grandes reduções dos níveis de vibração no rotor, quando comparado aos níveis de vibração do rotor original. Para a bancada de testes foram realizadas simulações adicionais, tendo em vista que o rotor experimental utiliza dois mancais magnéticos para levitar e controlar as vibrações. Foram apresentados os resultados de simulações de dois controladores LQR projetados com os dados da bancada de testes utilizada nos experimentos. O primeiro controlador considera modelo de rotor flexível modelado pelo método de elementos finitos e reduzido com a técnica de redução pseudo-modal. O segundo controlador foi modelado considerando o rotor como sendo um corpo rígido. Os resultados experimentais foram confrontados com os resultados de simulação e com os resultados obtidos do controlador do fabricante que forneceu a bancada
This paper deals with vibration control of rotors using active magnetic bearings. Numerical simulations were presented for the optimal positioning of a magnetic actuator used to attenuate vibrations in rotor supported by conventional bearings. The optimal positioning of the actuator was implemented using as objective function the norm H2 e H∞. To model the rotor was used finite element method (FEM) and the pseudo-modal reduction technique to reduce computational effort during the control. The simulations showed that a good positioning actuator combined to the control LQR provide great reductions in the levels of vibration in the rotor, compared the vibration of the original rotor. For the test rig were realized adittional simulations, in view of the rotor experimental uses two magnetic bearings for levitating and control the vibrations. Were present the results of two simulations designed LQR controllers with data from the test rig used in the experiments. The first controller model considers flexible rotor modeled by finite element method and reduced with the pseudo-modal reduction technique. The second controller is modeled considering the rotor as a rigid body. The experimental results were compared with simulation results and the results obtained from the controller manufacturer who supplied the test rig
Sino, Rim. "Comportement dynamique et stabilité des rotors : application aux rotors composites". Lyon, INSA, 2007. http://theses.insa-lyon.fr/publication/2007ISAL0067/these.pdf.
Pełny tekst źródłaThis work deals with the study of dynamic instabilities within rotating assemblies due to internal damping effects. In order to consider realistic mechanical properties, in terms of internal damping, a rheological model is associated to a general finite element beam approach, including transversal shear. After a description of the theoretical background (choice of internal damping model and equations of motion), a first application illustrates the ability of the proposed model. The influence of damping on frequencies and on instability thresholds is investigated using a parametric study. Results are compared to those obtained from an analytical approach as well as from experiments. A second application is concerned with the dynamic instability of an internally damped rotating composite shaft. A Simplified Homogenized Beam Theory (SHBT), which takes into account internal damping, is introduced and then used to evaluate natural frequencies and instability thresholds. The results are compared to those obtained by using an Equivalent Modulus Beam Theory (EMBT) widely used in the literature, a Modified Equivalent Modulus Beam Theory and a Layerwise Beam Theory (LBT). The influence of laminate parameters: stacking sequences, fiber orientation and transversal shear effect on natural frequencies and instability thresholds of the shaft is studied via a parametrical study. This parametric study shows that shaft instability thresholds can be very sensitive to all these parameters
Sino, Rim Jacquet-Richardet Georges. "Comportement dynamique et stabilité des rotors application aux rotors composites /". Villeurbanne : Doc'INSA, 2007. http://docinsa.insa-lyon.fr/these/pont.php?id=sino.
Pełny tekst źródłaJarroux, Clément. "Nonlinear transient dynamics of on-board rotors supported by Active Magnetic Bearings". Thesis, Lyon, 2017. http://www.theses.fr/2017LYSEI069/document.
Pełny tekst źródłaTurbomachines are rotating machines enabling the conversion of the different types of energy. The latter are composed of a rotating mechanical part, called rotor, interacting with a fluid. Therefore, rotation play a key role in these machines and the mechanical link between the fixed and the rotating parts, called bearing, is essential for reliable and optimal operations. Turbomachines supported by active magnetic bearings (AMBs) are increasingly used by industrial companies, especially thanks to the absence of direct contact between fixed and rotating parts, enabling energy savings and reduction of CO2 emissions. Most of the time, these machines are "on-board" and are fixed on mobile supports. The motions generated by these supports must be considered in the prediction of the dynamic behaviour of turbomachinery in order to improve the designs accordingly. This PhD is a contribution to the study of turbomachines supported by AMBs subjected to strong external base motions. The approach is numerical and experimental. The use of an academic scale test rig comprising a rotor-AMB system, with the properties of an industrial turbomachine, allowed to test the developed models for cases of external solicitations such as earthquake and shock, thanks to the 6-axis shaker of the equipex PHARE. It is shown that the model provides good predictions of the behaviour of the machine for the tested cases. This tool can therefore be used for industrial designs
Matos, Catherine Anne Moseley. "Download reduction on a wing-rotor configuation". Diss., Georgia Institute of Technology, 2001. http://hdl.handle.net/1853/12058.
Pełny tekst źródłaRigsby, James Michael. "Stability and control issues associated with lightly loaded rotors autorotating in high advance ratio flight". Diss., Atlanta, Ga. : Georgia Institute of Technology, 2008. http://hdl.handle.net/1853/26536.
Pełny tekst źródłaCommittee Chair: J.V.R. Prasad; Committee Member: Daniel P. Schrage; Committee Member: David A. Peters; Committee Member: Dewey H. Hodges; Committee Member: Lakshmi N Sankar. Part of the SMARTech Electronic Thesis and Dissertation Collection.
Akin, Hakki E. "A computer code for rapid calculation of bending frequencies of rotor blades". Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2002. http://library.nps.navy.mil/uhtbin/hyperion-image/02sep%5FAkin.pdf.
Pełny tekst źródłaThesis advisor(s): E. Roberts Wood, Mark A. Couch. Includes bibliographical references (p. 195-196). Also available online.
Atkinson, G. T. "Wind rotors in yaw". Thesis, University of Cambridge, 1987. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.384765.
Pełny tekst źródłaXie, Lihan. "Suivi numérique des bifurcations pour l'analyse paramétrique de la dynamique non-linéaire des rotors". Thesis, Lyon, 2016. http://www.theses.fr/2016LYSEI018/document.
Pełny tekst źródłaGenerally speaking, the rotating systems utilized in the energy production have a small rotor-stator gap, are able to run during long periods, and are mounted on hydrodynamic bearings. Rotor-stator interactions in case of blade loss, crack propagation due to fatigue, and a variable stiffness due to the nonlinear restoring forces of the bearings can make the rotordynamics nonlinear and the responses complicated: significant amplitude and frequency shifts are introduced, sub- and super-harmonics appear, and hysteresis occurs. It is of great importance to understand, predict and control this complicated dynamics. Due to the large number of DOFs and the broad range of study frequency, the computation time for solving the equations of motion by a temporal integration method can be quite prohibitive. It becomes particularly disadvantageous at the design stage where a parametrical study need to be quickly performed. An alternative numerical method, which is general and effective at the same time, is proposed in order to analyse the nonlinear response of the rotors at steady state. Firstly, the periodic responses of nonlinear rotors are calculated in the frequency domain by combining harmonic balance method (HBM) and alternating frequency-time (AFT). With the help of continuation method, all dynamic equilibrium solutions of nonlinear systems are determined for the range of study frequency. Then, Floquet exponents which are the eigenvalues of Jacobian are sought for stability analysis of periodic solutions. Then the local stability of the periodic solution is analysed through the bifurcation indicators which are based on the evolution of Floquet exponents. The bifurcations of periodic solution branch, such as limit point, branch point, and Neimark-Sacker bifurcation, are thus detected. By declaring a system parameter (friction coefficient, rotor / stator gap, excitation amplitude, ...) as a new variable, applying once again the continuation method to the augmented system determines directly the bifurcation's evolution as a function of this parameter. Thus, parametric analysis of the nonlinear dynamic behaviour is achieved, the stability boundary or the regime change boundary is directly determined. Numerous developments are implemented in the calculation code Cast3M
Viana, Serra Villa Cristiano. "Dynamique non linéaire des rotors : Applications numériques et expérimentales à un rotor flexible". Ecully, Ecole centrale de Lyon, 2005. http://bibli.ec-lyon.fr/exl-doc/cvilla.pdf.
Pełny tekst źródłaThis thesis deals with the dynamic behavior of rotating machinery containing the parts whose behavior is described by non linear laws. The first goal of this research is to implement methods of non linear analysis in order to solve the equations of motion of the system. Secondly, experimental studies are made with a test rig and the results are used to update a numeric model. The rotor is represented by a finite element model. To model the bearings, three models with different levels of complexity are presented, and a model where the kinematics of the rolling elements is adopted. The type of motion of interest is the steady state vibration, and to obtain this kind of solution it is advisable to use a frequential method like the Harmonic Balance Method Alternating Frequency Time (HBM AFT). This method can be implemented with an exact condensation strategy to reduce the computational time. The HBM AFT method is validated by comparing with a direct integration of a non linear Jeffcott rotor
Książki na temat "Rotors"
Ralph, Jolly J., Marcolini Michael A i United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. Helicopter main-rotor noise: Determination of source contributions using scaled model data. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Znajdź pełny tekst źródłaBrooks, Thomas F. Helicopter main-rotor noise: Determination of source contributions using scaled model data. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Znajdź pełny tekst źródłaBrooks, Thomas F. Helicopter main-rotor noise: Determination of source contributions using scaled model data. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Znajdź pełny tekst źródłaBrooks, Thomas F. Helicopter main-rotor noise: Determination of source contributions using scaled model data. Hampton, Va: Langley Research Center, 1988.
Znajdź pełny tekst źródłaBachschmid, Nicolò, Paolo Pennacchi i Ezio Tanzi. Cracked Rotors. Berlin, Heidelberg: Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-642-01485-7.
Pełny tekst źródłaGilliand, Harry E. Dancing rotors. Arlington, Tex: Aerofax, 1994.
Znajdź pełny tekst źródłaGanguli, Ranjan, Dipali Thakkar i Sathyamangalam Ramanarayanan Viswamurthy. Smart Helicopter Rotors. Cham: Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-24768-7.
Pełny tekst źródłaMutza, Wayne. Bent & battered rotors. Carrollton, TX: Squadron/Signal Publications, 1993.
Znajdź pełny tekst źródłaRunyan, Harry L. Compressible, unsteady lifting-surface theory for a helicopter rotor in forward flight. Washington: NASA, 1985.
Znajdź pełny tekst źródłaH, Tai, i United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., red. Compressible, unsteady, lifting-surface theory for a helicopter rotor in forward flight. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Znajdź pełny tekst źródłaCzęści książek na temat "Rotors"
Bachschmid, Nicolò, Paolo Pennacchi i Ezio Tanzi. "Cracks in Rotating Shafts". W Cracked Rotors, 1–15. Berlin, Heidelberg: Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-642-01485-7_1.
Pełny tekst źródłaBachschmid, Nicolò, Paolo Pennacchi i Ezio Tanzi. "Typical Dynamic Behaviour of Cracked Shafts". W Cracked Rotors, 17–35. Berlin, Heidelberg: Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-642-01485-7_2.
Pełny tekst źródłaBachschmid, Nicolò, Paolo Pennacchi i Ezio Tanzi. "Rotor Testing for Crack Detection". W Cracked Rotors, 37–90. Berlin, Heidelberg: Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-642-01485-7_3.
Pełny tekst źródłaBachschmid, Nicolò, Paolo Pennacchi i Ezio Tanzi. "Laboratory Tests on Cracked Shafts". W Cracked Rotors, 91–107. Berlin, Heidelberg: Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-642-01485-7_4.
Pełny tekst źródłaBachschmid, Nicolò, Paolo Pennacchi i Ezio Tanzi. "Crack Modelling". W Cracked Rotors, 109–98. Berlin, Heidelberg: Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-642-01485-7_5.
Pełny tekst źródłaBachschmid, Nicolò, Paolo Pennacchi i Ezio Tanzi. "Results Obtained Using Simulations". W Cracked Rotors, 199–246. Berlin, Heidelberg: Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-642-01485-7_6.
Pełny tekst źródłaBachschmid, Nicolò, Paolo Pennacchi i Ezio Tanzi. "Some Special Effects Caused by Cracks". W Cracked Rotors, 247–301. Berlin, Heidelberg: Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-642-01485-7_7.
Pełny tekst źródłaBachschmid, Nicolò, Paolo Pennacchi i Ezio Tanzi. "Crack Diagnosis in Rotating Shafts". W Cracked Rotors, 303–94. Berlin, Heidelberg: Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-642-01485-7_8.
Pełny tekst źródłaDimarogonas, A., i A. Kollias. "Smart Rotors". W Rotordynamics ’92, 100–106. London: Springer London, 1992. http://dx.doi.org/10.1007/978-1-4471-1979-1_13.
Pełny tekst źródłaVince, John. "Bivector Rotors". W Rotation Transforms for Computer Graphics, 181–96. London: Springer London, 2011. http://dx.doi.org/10.1007/978-0-85729-154-7_12.
Pełny tekst źródłaStreszczenia konferencji na temat "Rotors"
Marin, Manuel A. "Rotor Dynamics of Overhung Rotors: Hysteretic Dynamic Behavior". W ASME Turbo Expo 2012: Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/gt2012-68285.
Pełny tekst źródłaCarroll, Tim, Issi-Rae E. George i Goetz Bramesfeld. "Design Optimization of Small Rotors in Quad-Rotor Configuration". W 54th AIAA Aerospace Sciences Meeting. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2016. http://dx.doi.org/10.2514/6.2016-1788.
Pełny tekst źródłaAlasty, Aria, i Mohammad Malekian. "Identification of Distributed Unbalanced Mass in Flexible Rotors". W ASME 8th Biennial Conference on Engineering Systems Design and Analysis. ASMEDC, 2006. http://dx.doi.org/10.1115/esda2006-95160.
Pełny tekst źródłaFilali, Abdelkader, Lyes Khezzar i Hamza Semmari. "Improved Power for Wind Farm Savonius Rotors: Effect of Blade Shape and Rotors Position". W ASME 2020 Fluids Engineering Division Summer Meeting collocated with the ASME 2020 Heat Transfer Summer Conference and the ASME 2020 18th International Conference on Nanochannels, Microchannels, and Minichannels. American Society of Mechanical Engineers, 2020. http://dx.doi.org/10.1115/fedsm2020-20071.
Pełny tekst źródłaIbrahim, Ahmed, i Ahmed M. R. Elbaz. "Investigating Efficient Clusters of Savonius Wind Turbines". W ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2018. http://dx.doi.org/10.1115/gt2018-75405.
Pełny tekst źródłaMiesner, Sebastian, Manuel Kessler i Ewald Kramer. "High-fidelity Simulations of Rotors in Compact Configuration". W Vertical Flight Society 78th Annual Forum & Technology Display. The Vertical Flight Society, 2022. http://dx.doi.org/10.4050/f-0078-2022-17466.
Pełny tekst źródłaAtte, Abraham, i Huergen Rauleder. "Investigation of Rotor Vertical Offset Effects on Quadrotor Performance". W Vertical Flight Society 80th Annual Forum & Technology Display. The Vertical Flight Society, 2024. http://dx.doi.org/10.4050/f-0080-2024-1388.
Pełny tekst źródłaDayhoum, Abdallah, Alejandro Ramirez-Serrano i Robert Martinuzzi. "Aerodynamic Optimization and Experimental Analysis of Shrouded Rotor Blades". W Vertical Flight Society 80th Annual Forum & Technology Display. The Vertical Flight Society, 2024. http://dx.doi.org/10.4050/f-0080-2024-1289.
Pełny tekst źródłaBaz, Ahmed M., Nabil A. Mahmoud, Ashraf M. Hamed i Khaled M. Youssef. "Optimization of Two and Three Rotor Savonius Wind Turbine". W ASME Turbo Expo 2015: Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2015. http://dx.doi.org/10.1115/gt2015-43988.
Pełny tekst źródłaReddinger, Jean-Paul. "Coupled Pitch-Lag Hinge for High Inertia Electric Rotors". W Vertical Flight Society 76th Annual Forum & Technology Display. The Vertical Flight Society, 2020. http://dx.doi.org/10.4050/f-0076-2020-16327.
Pełny tekst źródłaRaporty organizacyjne na temat "Rotors"
Zheng, Wanzheng, i Jason Merret. Aerodynamic Survey of Novel eVTOL Configuration Using SU2. Illinois Center for Transportation, sierpień 2022. http://dx.doi.org/10.36501/0197-9191/22-014.
Pełny tekst źródłaSmith, A. B. Fast neutrons incident on rotors : - tantalum. Office of Scientific and Technical Information (OSTI), marzec 2005. http://dx.doi.org/10.2172/861625.
Pełny tekst źródłaRomero, Louis Anthony. Spin stabilized magnetic levitation of horizontal rotors. Office of Scientific and Technical Information (OSTI), październik 2004. http://dx.doi.org/10.2172/882322.
Pełny tekst źródłaBortolotti, Pietro, Emmanuel Branlard, Anurag Gupta, Nick Johnson, Jason Jonkman, Patrick Moriarty, Joshua Paquette, Dave Snowberg i Paul Veers. The Wind Turbine Rotors of the Future: A Research Agenda from the Big Adaptive Rotor Project. Office of Scientific and Technical Information (OSTI), maj 2024. http://dx.doi.org/10.2172/2356775.
Pełny tekst źródłaManiaci, David Charles, Christopher Lee Kelley i Phillip Chiu. Assessment of Scaled Rotors for Wind Tunnel Experiments. Office of Scientific and Technical Information (OSTI), lipiec 2015. http://dx.doi.org/10.2172/1235645.
Pełny tekst źródłaMorino, Luigi, Slobodan Sipcic i Mark Downey. Unsteady Free-Wake Viscous Aerodynamic Analysis of Helicopter Rotors. Fort Belvoir, VA: Defense Technical Information Center, listopad 1989. http://dx.doi.org/10.21236/ada217166.
Pełny tekst źródłaLoth, Eric. 50 MW SEGMENTED ULTRALIGHT MORPHING ROTORS FOR WIND ENERGY. Office of Scientific and Technical Information (OSTI), czerwiec 2024. http://dx.doi.org/10.2172/2375003.
Pełny tekst źródłaCheney, M. C., T. Olsen, G. Quandt i P. Archidiacono. Analysis and Tests of Pultruded Blades for Wind Turbine Rotors. Office of Scientific and Technical Information (OSTI), lipiec 1999. http://dx.doi.org/10.2172/12142.
Pełny tekst źródłaBlau, Peter Julian. Prospects for Titanium-Based Materials as Truck Disc Brake Rotors. Office of Scientific and Technical Information (OSTI), wrzesień 2010. http://dx.doi.org/10.2172/1081592.
Pełny tekst źródłaShiu, Henry, i Cornelis P. van Dam. Active Flow Control on Bidirectional Rotors for Tidal MHK Applications. Office of Scientific and Technical Information (OSTI), sierpień 2013. http://dx.doi.org/10.2172/1090896.
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