Aerodynamics

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Aerodynamics is a branch of dynamics concerned with studying the motion of air, particularly when it interacts with a moving object. (Wikipedia.org)






Conferences related to Aerodynamics

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2019 IEEE International Electric Machines & Drives Conference (IEMDC)

The IEEE International Electric Machines and Drives Conference (IEMDC) has been established to be one of the major events in the field of electrical machines and drives. IEMDC is a refernce forum to disseminate and exchange state of art in the filed of the Electrical Machines and Drives. The 2018 edition started in 1997 and the 2019 edition will be 11th one.


2019 IEEE Pulsed Power & Plasma Science (PPPS)

Combined conference of the IEEE International Conference on Plasma Science and the IEEE International Pulsed Power Conference


2018 13th IEEE Conference on Industrial Electronics and Applications (ICIEA)

Industrial Informatics, Computational Intelligence, Control and Systems, Cyber-physicalSystems, Energy and Environment, Mechatronics, Power Electronics, Signal and InformationProcessing, Network and Communication Technologies


2018 19th Electromagnetic Launch Technology Conference (EML)

All aspects concerning electromagnetic launch are going to be discussed.


2018 20th European Conference on Power Electronics and Applications (EPE'18 ECCE Europe)

Energy conversion and conditioning technologies, power electronics, adjustable speed drives and their applications, power electronics for smarter grid, energy efficiency,technologies for sustainable energy systems, converters and power supplies


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Periodicals related to Aerodynamics

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Aerospace and Electronic Systems Magazine, IEEE

The IEEE Aerospace and Electronic Systems Magazine publishes articles concerned with the various aspects of systems for space, air, ocean, or ground environments.


Antennas and Wireless Propagation Letters, IEEE

IEEE Antennas and Wireless Propagation Letters (AWP Letters) will be devoted to the rapid electronic publication of short manuscripts in the technical areas of Antennas and Wireless Propagation.


Automatic Control, IEEE Transactions on

The theory, design and application of Control Systems. It shall encompass components, and the integration of these components, as are necessary for the construction of such systems. The word `systems' as used herein shall be interpreted to include physical, biological, organizational and other entities and combinations thereof, which can be represented through a mathematical symbolism. The Field of Interest: shall ...


Communications Magazine, IEEE

IEEE Communications Magazine was the number three most-cited journal in telecommunications and the number eighteen cited journal in electrical and electronics engineering in 2004, according to the annual Journal Citation Report (2004 edition) published by the Institute for Scientific Information. Read more at http://www.ieee.org/products/citations.html. This magazine covers all areas of communications such as lightwave telecommunications, high-speed data communications, personal communications ...


Computer

Computer, the flagship publication of the IEEE Computer Society, publishes peer-reviewed technical content that covers all aspects of computer science, computer engineering, technology, and applications. Computer is a resource that practitioners, researchers, and managers can rely on to provide timely information about current research developments, trends, best practices, and changes in the profession.


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Most published Xplore authors for Aerodynamics

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Xplore Articles related to Aerodynamics

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Comparison of BEM and Full Navier-Stokes CFD Methods for Prediction of Aerodynamics Performance of HAWT Rotors

[{u'author_order': 1, u'affiliation': u'Ecole Nationale Polytechnique, Mechanical Engineering and Development Laboratory, Alger, 16200, Algeria', u'full_name': u'Abdelhamid Bouhelal'}, {u'author_order': 2, u'affiliation': u'Ecole Nationale Polytechnique, Mechanical Engineering and Development Laboratory, Alger, 16200, Algeria', u'full_name': u'Arezki Smaili'}, {u'author_order': 3, u'affiliation': u'Centre de Développement des Énergies Renouvelables, Bouzaréah, Alger, Alegria', u'full_name': u'Ouahiba Guerri'}, {u'author_order': 4, u'affiliation': u'Ecole de Technologie Supérieure, Department of Mechanical Engineering, Montréal, Québec, Canada', u'full_name': u'Christian Masson'}] 2017 International Renewable and Sustainable Energy Conference (IRSEC), None

The essential contribution of this study consists of comparing between two radically different aerodynamic methods which were applied to predict the aerodynamic performance of horizontal axis wind turbines (HAWTs). The classical blade element momentum theory (BEM) and full rotor geometry computational fluid dynamics (CFD) based on the Reynolds Averaged Navier- Stokes (RANS) approach were used in order to discover their ...


Overview of ONERA Fluidic Actuators in Aerodynamics

[{u'author_order': 1, u'full_name': u'F. Ternoy'}, {u'author_order': 2, u'full_name': u'E. Eglinger'}, {u'author_order': 3, u'full_name': u'J. Dandois'}, {u'author_order': 4, u'full_name': u'J. Delva'}] ACTUATOR 2018; 16th International Conference on New Actuators, None

In aerodynamics fluidic actuators are used to modify the main flow around vehicles by injecting a secondary flow on its surface through slots or holes. The interaction of this secondary flow aims at improving the aerodynamic performance of the vehicle. Today, in most of the cases, numerical simulations allow to follow the evolution of all flow variables in the external ...


Wall Temperature Effects on Hypersonic Aerodynamics of the Mars Entry Capsule

[{u'author_order': 1, u'affiliation': u'School of Aeronautic Science and Engineering, Beihang University, Beijing, China', u'full_name': u'Kang Zhong'}, {u'author_order': 2, u'affiliation': u'School of Aeronautic Science and Engineering, Beihang University, Beijing, China', u'full_name': u'Xiaoyong Wang'}, {u'author_order': 3, u'affiliation': u'School of Aeronautic Science and Engineering, Beihang University, Beijing, China', u'full_name': u'Chao Yan'}] 2018 9th International Conference on Mechanical and Aerospace Engineering (ICMAE), None

The chemical non-equilibrium method is implemented to investigate wall temperature effects on the hypersonic aerodynamics of the Mars entry capsule named Mars Science Laboratory (MSL). Two isothermal walls (1000 and 2000K) and a radiative-equilibrium wall temperature are used to take account of the temperature effects, respectively. The numerical results show that, the wall temperature has no significant effect on the ...


Optimizations of Unstructured Aerodynamics Computations for Many-core Architectures

[{u'author_order': 1, u'affiliation': u'Extreme Computing Research Center, King Abdullah University of Science and Technology, Thuwal, Saudi Arabia', u'full_name': u'Mohammed A. Al Farhan'}, {u'author_order': 2, u'affiliation': u'Extreme Computing Research Center, King Abdullah University of Science and Technology, Thuwal, Saudi Arabia', u'full_name': u'David E. Keyes'}] IEEE Transactions on Parallel and Distributed Systems, 2018

We investigate several state-of-the-practice shared-memory optimization techniques applied to key routines of an unstructured computational aerodynamics application with irregular memory accesses. We illustrate for the Intel Knights Landing processor, as a representative of the processors in contemporary leading supercomputers, identifying and addressing performance challenges without compromising the floating point numerics of the original code. We employ low and high-level architecture-specific ...


An Aerodynamics-Based Novel Optimal Power Extraction Strategy for Offshore Wind Farms With Central VSCs

[{u'author_order': 1, u'affiliation': u'School of Automation, Guangdong University of Technology, Guangzhou, China', u'full_name': u'Si-Zhe Chen'}, {u'author_order': 2, u'affiliation': u'School of Automation, Guangdong University of Technology, Guangzhou, China', u'full_name': u'Guozhuan Xiong'}, {u'author_order': 3, u'affiliation': u'School of Automation, Guangdong University of Technology, Guangzhou, China', u'full_name': u'Guidong Zhang'}, {u'author_order': 4, u'affiliation': u'School of Electrical, Electronics, and Computer Engineering, The University of Western Australia, Perth, WA, Australia', u'full_name': u'Samson Shenglong Yu'}, {u'author_order': 5, u'affiliation': u'School of Electrical, Electronics, and Computer Engineering, The University of Western Australia, Perth, WA, Australia', u'full_name': u'Ho-Ching Iu'}, {u'author_order': 6, u'affiliation': u'School of Electrical, Electronics, and Computer Engineering, The University of Western Australia, Perth, WA, Australia', u'full_name': u'Tyrone Fernando'}, {u'author_order': 7, u'affiliation': u'School of Automation, Guangdong University of Technology, Guangzhou, China', u'full_name': u'Yun Zhang'}] IEEE Access, 2018

Costly distributed converters are used in traditional offshore wind turbine generators (WTGs); recently, centralized voltage source converters (CVSC) have been utilized to replace the distributed ones for cost reduction. This method, however, reduces the wind energy that can be harvested from the environment, since all WTGs' synchronous rotational speeds depend on the frequency of the same CVSC but their wind ...


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Educational Resources on Aerodynamics

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eLearning

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IEEE.tv Videos

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IEEE-USA E-Books

  • Computational Electromagnetic-Aerodynamics

    Computational electromagnetic-aerodynamics (CEA) or computational electromagnetic fluid dynamics is an interdisciplinary science. The fundamental governing equations are the Boltzmann and Maxwell equations for describing the plasma dynamics in flow fields. The system of equations solves distribution functions of space and velocity in time that is a seven- dimensional formulation, and solutions to the governing equations are probabilistic. In cases the collision mean-free path is much greater than the characteristic scale of the studied phenomenon, the plasma can be approximated as collisionless and the Vlasov approximation is valid. The chapter discusses unique feature of diffusion in plasma and additional and uncommon mechanisms such as pressure, thermal, field force diffusion other than the electromagnetic field. In summary, most adopted numerical algorithms in CEA are shared with CFD, especially for thermally excited ionizations. These numerical procedures are built on either the classical ADI scheme for finite- difference approximation or the Gauss-Siedel relaxation for finite-volume approach.

  • Aerodynamics of Aircraft in Maneuver

    This chapter contains sections titled: 6.1 Aircraft Motion Definition, 6.2 Axis Systems, 6.3 Non-Dimensionalization and Parameterization, 6.4 Lifting Surface Theory, 6.5 Vortex Lattice Method, 6.6 Slender Body Theory

  • Bicycle aerodynamics

    This chapter contains sections titled: Introduction, Drag coefficient, Drag, Reducing the aerodynamic drag of bicycles, Other aerodynamic phenomena, References, Recommended reading

  • Joule-Heating Actuators

    Many exciting innovations were put forth in areas of Magnetohydrodynamics (MHD) propulsion, remote energy deposition for drag reduction, plasma actuator, radiation-driven hypersonic wind tunnel, sonic boom meditation, and enhanced plasma ignition and combustion stability. The plasma heating consists mainly of Joule-heating and stochastic heating; the latter however is nearly negligible except in an oscillating plasma sheath. The Joule-heating concentrates within the cathode layer and is a rather small but effective spatial heat source to the surrounding gas stream. The interactions between aerodynamics and the surface electron impact discharge have been simulated by computational electromagnetic aerodynamics using a multifluid, drift-diffusion weakly ionized gas model. Surface pressures were recorded for a variety of magnetic field strengths and electric currents for all combinations of electrode and magnet polarity. Small perturbations in a boundary layer by a shallow bump can produce a profound change to the dynamic structure of a flow field.

  • Computational Fluid Dynamics

    A wide range of coordinate transformation techniques, computational grid generations, and different grid topologies have also been devised to accommodate complex aerodynamic configurations. This chapter focuses on computational fluid dynamics and the electromagnetic-aerodynamics interactions are addressed. The fundamental principle of Newtonian mechanics is the conservation of mass, which means that the exchange of mass and energy is not considered. Classic viscous-inviscid interactions without flow separation are noted on leading edges of an aerodynamic shape from vorticity and Mach wave interactions. The self-sustained oscillation is evident and the magnitude of the pressure pulsation is about 17 times of the free stream value. Vortex bifurcations at high incidence drastically affect aerodynamic behavior embracing asymmetric forebody vortex formation, vortex breakdown, and unsteady asymmetric force generation. Laminar-turbulent transition is one of the most challenging of fluid dynamics phenomena because it is a nonlinear and time- dependent fluid dynamic bifurcation and deeply rooted in hydrodynamic stability.

  • Lorentz-Force Actuator

    This chapter discusses the remote energy deposition through plasma injection or a microwave beam, and the resulting stagnation point heat transfer mitigation. An outstanding feature of plasma in an extremely strong externally applied magnetic field is that the magnetic lines are frozen in charged particle motion. An idealized upper theoretical limit for stagnation point heat transfer mitigation is demonstrated by Gaitonde and Poggie by solving the MHD equations with a value of electric conductivity determined by a square power-law dependence to local temperature. The computational results produce only the periodic electrostatic force of the direct current discharge (DBD), which is the driving mechanism of the electric wind, but the experimental data are the measured resultant force through the interaction of the charged and neutral particles. A numerical simulation of micro jets will definitely open a new avenue for research into enhancing combustion stability, plasma-assisted ignition, and wound pathologies.

  • Plasma Fundamentals

    No Abstract.

  • Ionization Processes

    The ionization process of atoms or molecules is through energizing the electrons causing them to leave stable orbit revolving around the nucleus and becoming free-moving charges. The main mechanisms for ionization consist of thermal, electron impact, chemical reactions, photoionization, and microwave or electron cyclotron resonance. This chapter describes the ionization that focus on the basic mechanisms of photoemission, thermal, and electron impact discharges. The equilibrium ionization of the mixture of electrons, ions, and neutral particles can be analyzed by the law of mass action and the electronic partition function. Under gas discharge conditions, ionization by electron impact dominates over the photoionization because the cross sections of photoionization close to the ionizing threshold are rather high. The chapter provides Saha equation of ionization. An important parameter for the ionization rate is the mean free path of the gas medium and is ultimately related to the collision cross section.

  • Front Matter

    The prelims comprise: * Half Title * Title * Copyright * Contents * Preface

  • Magnetohydrodynamics Formulation

    Magnetohydrodynamics (MHD) was originally applied mostly to astrophysics and geophysics. In MHD the motion of collective charged particles is described by an electrically conducting fluid with the usual fluid dynamic variables of velocity, density and pressure or temperature. The interactions of fluid dynamics and electromagnetics are exclusively derived from the magnetic flux density. This chapter presents a systematic derivation of the governing equations of MHD. The first and foremost assumption for MHD formulation is that the physical phenomena are describable by macroscopic scales or in the framework of continuum mechanics. The electromagnetic waves are compound waves for which the compression and rarefaction components can coexist and the direct consequence of the nonconvexity of the ideal MHD equations. The chapter discusses additional computational simulations to show the lack of detailed plasma composition that is required for determining electric conductivity of plasma in the MHD formulation.



Standards related to Aerodynamics

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