Thematische Bibliographien / European Computational Aerodynamics Research Project

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Auswahl der wissenschaftlichen Literatur zum Thema „European Computational Aerodynamics Research Project“

Autor: Grafiati

Veröffentlicht am 4. Juni 2021

Zuletzt aktualisiert am 29. Juli 2025

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Zeitschriftenartikel zum Thema "European Computational Aerodynamics Research Project"

Shaw, J. A. "Computational Mesh Adaption: ECARP – European Computational Aerodynamics Research Project D.P. Hillset al. Vieweg Publishing, PO Box 5829, D65048 Wiesbaden, Germany. 1999. 285pp. Illustrated. ISBN 3-528-06969-4." Aeronautical Journal 105, no. 1046 (2001): 230. http://dx.doi.org/10.1017/s0001924000025483.

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Bermejo, Oscar, Juan Manuel Gallardo, Adrian Sotillo, Arnau Altuna, Roberto Alonso, and Andoni Puente. "Numerical and Experimental Study of Flutter in a Realistic Labyrinth Seal." International Journal of Turbomachinery, Propulsion and Power 9, no. 2 (2024): 13. http://dx.doi.org/10.3390/ijtpp9020013.

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Labyrinth seals are commonly used in turbomachinery in order to control leakage flows. Flutter is one of the most dangerous potential issues for them, leading to High Cycle Fatigue (HCF) life considerations or even mechanical failure. This phenomenon depends on the interaction between aerodynamics and structural dynamics; mainly due to the very high uncertainties regarding the details of the fluid flow through the component, it is very hard to predict accurately. In 2014, as part of the E-Break research project funded by the European Union (EU), an experimental campaign regarding the flutter b

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Dexter, P. C. "A strategic European approach to aerodynamics research, technology and development." Aeronautical Journal 105, no. 1050 (2001): 451–57. http://dx.doi.org/10.1017/s0001924000012434.

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Abstract In spite of the best intentions of many national and international funding agencies, much of the research and technology development (RTD) activity undertaken in Europe over the past few years has often been duplicating the work of others and has not resulted in an increase in capability in key areas. This is not to denigrate the work that has been undertaken — but have we done the right work? The EC-funded Thematic Network ‘Targeted Research Action in Aerospace Aerodynamics’, (TRA3), has been initiated with the broad aims of improving collaboration between existing EC- supported proj

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Van Hinsberg, Nils Paul, Ulrich Henne, and Christian Klein. "Application Of Temperature-Sensitive Paint For Transition Detection On An NLF Forward-Swept Wing Under Harmonic Pitch Oscillation At Flight-Relevant Mach And Reynolds Numbers." Proceedings of the International Symposium on the Application of Laser and Imaging Techniques to Fluid Mechanics 21 (July 8, 2024): 1–30. http://dx.doi.org/10.55037/lxlaser.21st.156.

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To reduce the fuel consumption and emissions of next generation commercial aircraft, the highly promising natural laminar flow (NLF) technology is being implemented more and more frequently. By maintaining a laminar flow over the largest possible area of both wings through either passive or active measures, the overall aircraft friction drag over these surfaces can be significantly reduced, which results in a distinct increase in the aerodynamic performance of the aircraft. To raise the Technology Readiness Level of this laminar technology in aircraft design, an NLF forward-swept wing fuselage

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Kumar, Gaurav, Rohit Kumar, Sagar Dagar, and Raj Kumar Singh. "Comparative Study of Different Missile Shapes using Computational Fluid Dynamics." International Journal of Advance Research and Innovation 8, no. 3 (2020): 72–83. http://dx.doi.org/10.51976/ijari.832012.

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Aerodynamics study using computational fluid dynamics is very famous among the engineers and scientists, because it not only reduces the cost of the entire project but also saves a lot more time. The results of the CFD simulations needed to validate through experiments. So, we can say that CFD simulation studies reduce the no. Of experiments taken, if it cannot eliminate. In this research paper, we made four different aerodynamics missiles shapes CAD models in solid works by using underlying principles, mathematical equations of different curves and engineering judgement, one of them is a miss

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Mendonça, Gonçalo, Frederico Afonso, and Fernando Lau. "Model order reduction in aerodynamics: Review and applications." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233, no. 15 (2019): 5816–36. http://dx.doi.org/10.1177/0954410019853472.

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The need of the aerospace industry, at national or European level, of faster yet reliable computational fluid dynamics models is the main drive for the application of model reduction techniques. This need is linked to the time cost of high-fidelity models, rendering them inefficient for applications like multi-disciplinary optimization. With the goal of testing and applying model reduction to computational fluid dynamics models applicable to lifting surfaces, a bibliographical research covering reduction of nonlinear, dynamic, or steady models was conducted. This established the prevalence of

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Goraj, Zdobyslaw. "UCAV PW-124 – A DESIGN EFFORT UNDERTAKEN AT WARSAW UNIVERSITY OF TECHNOLOGY." Aviation 9, no. 4 (2005): 3–15. http://dx.doi.org/10.3846/16487788.2005.9635912.

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This paper presents a conceptual design project developed at the Warsaw University of Technology and focused on an unmanned aerial vehicle being able to fly at low and medium altitude, with a special emphasis put on selecting the platform best suited for the planned mission. Design and research activity necessary to complete the project successfully is based on the international experience gained by the university team within a number of the past very successful projects, mainly projects supported by European Union within the V and VI scientific frameworks. The project deals with a highly mane

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Kintscher, Markus, Johannes Riemenschneider, Hans-Peter Monner, and Martin Wiedemann. "Structural concept of an adaptive shock control bump spoiler." CEAS Aeronautical Journal 12, no. 3 (2021): 509–18. http://dx.doi.org/10.1007/s13272-021-00507-9.

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AbstractDrag reduction technologies in aircraft design are the key enabler for reducing emissions and for sustainable growth of commercial aviation. Laminar wing technologies promise a significant benefit by drag reduction and are, therefore, under investigation in various European projects. However, of the established moveable concepts and high-lift systems thus far most do not cope with the requirements for natural laminar flow wings. To this aim, new leading edge high-lift systems have been the focus of research activities in the last 5 years. Such leading edge devices investigated in proje

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Allen, C. B. "CHIMERA volume grid generation within the EROS code." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 214, no. 3 (2000): 125–41. http://dx.doi.org/10.1243/0954410001531962.

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The EROS (European ROtorcraft Software) project was a three-year, European Commission funded, collaborative project between research institutes, universities and industry, with the goal of producing a practical computational fluid dynamic (CFD)-based design tool for rotor blade design. The overlapping mesh, or CHIMERA, approach was adopted for structured grid generation within the project. The specifics of volume grid generation in GEROS, the EROS grid generator, are presented here. The capabilities and effectiveness of GEROS are demonstrated, and sample grids are shown for fixed-wing hovering

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Schultz, K. J., W. Splettstoesser, B. Junker, et al. "A parametric windtunnel test on rotorcraft aerodynamics and aeroacoustics (Helishape) — test procedures and representative results." Aeronautical Journal 101, no. 1004 (1997): 143–54. http://dx.doi.org/10.1017/s0001924000066483.

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Within the framework of a major European co-operative research project on rotorcraft aerodynamics and acoustics (Helishape), a parametric model rotor test was conducted in the open test section of the DNW using DLR's MWM test rig, and a highly instrumented model of a fully articulated ECF rotor equipped with blades of advanced design with two exchangeable blade tips. One set of blade tips (7A) was rectangular, while the other (7AD1) was a swept-back parabolic-anhedral shape. The objectives of this experimental research were to evaluate noise reduction techniques (conceptionally by variation of

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Bücher zum Thema "European Computational Aerodynamics Research Project"

P, Hills David, European Computational Aerodynamics Research Project., and European Commission. Directorate-General XII, Science, Research, and Development., eds. Computational mesh adaptation: ECARP--European Computational Aerodynamics Research Project. Vieweg, 1999.

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Jacques, Periaux, European Computational Aerodynamics Research Project., and European Commission. Directorate-General XII, Science, Research, and Development., eds. Optimum aerodynamic design & parallel Navier-Stokes computations: ECARP, European Computational Aerodynamics Research Project. Vieweg, 1998.

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Periaux, Jacques. Optimum Aerodynamic Design & Parallel Navier-Stokes Computations ECARP - European Computational Aerodynamics Research Project. Vieweg+Teubner Verlag, 1998.

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Periaux, Jacques, Gabriel Bugeda, Panagiotis K. Chaviaropoulos, Kyriakos Giannakoglou, Stephane Lanteri, and Bertrand Mantel, eds. Optimum Aerodynamic Design & Parallel Navier-Stokes Computations ECARP — European Computational Aerodynamics Research Project. Vieweg+Teubner Verlag, 1998. http://dx.doi.org/10.1007/978-3-322-90193-4.

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1945-, Haase W., European Computational Aerodynamics Research Project., and European Commission. Directorate-General XII, Science, Research, and Development., eds. ECARP: European Computational Aerodynamics Research Project : validation of CFD codes and assessment of turbulence models. Vieweg, 1997.

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Kroll, Norbert. ADIGMA - A European initiative on the development of adaptive higher-order variational methods for aerospace applications: Results of a collaborative research project funded by the European Union, 2006-2009. Springer, 2010.

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1945-, Haase W., ed. FLOMANIA: A European initiative on flow physics modelling : results of the European-Union funded project, 2002-2004. Springer, 2006.

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1945-, Haase W., ed. FLOMANIA: A European initiative on flow physics modelling : results of the European-Union funded project, 2002-2004. Springer, 2006.

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1945-, Haase W., ed. FLOMANIA: A European initiative on flow physics modelling : results of the European-Union funded project, 2002-2004. Springer, 2006.

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E, Stanewsky, ed. Drag reduction by shock and boundary layer control: Results of the project EUROSHOCK II supported by the European Union, 1996-1999. Springer, 2002.

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Buchteile zum Thema "European Computational Aerodynamics Research Project"

Alam, Sadaf, Javier Bartolome, Sanzio Bassini, et al. "Fenix: Distributed e-Infrastructure Services for EBRAINS." In Lecture Notes in Computer Science. Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-82427-3_6.

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AbstractThe Human Brain Project (HBP) (https://humanbrainproject.eu/) is a large-scale flagship project funded by the European Commission with the goal of establishing a research infrastructure for brain science. This research infrastructure is currently being realised and will be called EBRAINS (https://ebrains.eu/). The wide ranging EBRAINS services for the brain research communities require diverse access, processing and storage capabilities. As a result, it will strongly rely on e-infrastructure services. The HBP led to the creation of Fenix (https://fenix-ri.eu/), a collaboration of five

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Neves, Isabel Clara. "Digital Processes to Conscious Innovation in Built Environment." In Lecture Notes in Civil Engineering. Springer Nature Singapore, 2025. https://doi.org/10.1007/978-981-96-4749-1_35.

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Abstract Some 15 years ago, the world’s urban population surpassed the global rural population, an unprecedented shift in how and where we live. It is believed that by 2050 more than two thirds of the world’s population will be living in urban settings. How can, and should we integrate such a population into the project methodology, aiming at their participation? There has been a growing interest in increasing user commitment in conception design processes for built space, moving against fully top-down approaches. In turn, Research Centres have become increasingly interested in the potential o

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Konferenzberichte zum Thema "European Computational Aerodynamics Research Project"

Kus, Adrian, Sascha Schneider, Martin Hollands, Raphael Rammer, Oliver Dieterich, and Martijn Priems. "GRC1: An Advanced Five-Bladed Bearingless Main Rotor Dynamics and Acoustics from Draft to Flight Test." In Vertical Flight Society 74th Annual Forum & Technology Display. The Vertical Flight Society, 2018. http://dx.doi.org/10.4050/f-0074-2018-12754.

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Funded by the European research program Clean Sky Green Rotorcraft (GRC), a new five-bladed bearingless main rotor demonstrator has been developed and tested between 2014 and 2016 at Airbus Helicopters, hereafter denoted as GRC1 rotor. While inheriting rotor controls, control cuff, flexbeam and lead-lag damper from the Bluecopter™ main rotor, the rotor blade itself was developed from scratch within the research project. Main target was to achieve an ecofriendly design by simultaneously reducing acoustic signature, fuel consumption and vibratory loads while optimizing manufacturing costs. This

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Shirazi, Dorsa, Nicholas Peters, Carl Russell, et al. "Leveraging Modeling and Sensitivity Studies for Improving Aerodynamic Predictions for Multirotor Aircraft." In Vertical Flight Society 81st Annual Forum and Technology Display. The Vertical Flight Society, 2025. https://doi.org/10.4050/f-0081-2025-57.

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The NASA Revolutionary Vertical Lift Technology project aims to support and guide the development of vertical flight vehicles for the benefit of the U.S. rotorcraft community and to increase the quality of life of the public. As part of this effort, the Multirotor Test Bed (MTB) – designed and built by NASA – has been tested twice at the U.S. Army 7- by 10-Foot Wind Tunnel at NASA Ames Research Center in 2019 (MTB1) and 2022 (MTB2). This study utilizes MTB2 experimental data for sensitivity studies on rotor aerodynamic performance of a quadrotor configuration using two mid-fidelity tools, the

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Bermejo, Oscar, Juan Manuel Gallardo, Adrian Sotillo, Arnau Altuna, Roberto Alonso, and Andoni Puente. "Analytical, Numerical and Experimental Study of Flutter in a Realistic Labyrinth Seal." In ASME Turbo Expo 2023: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2023. http://dx.doi.org/10.1115/gt2023-101907.

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Abstract Labyrinth seals are frequently used in modern turbomachinery in order to control leakage flows between static and rotating elements. Previous experiences have demonstrated that flutter is a potential risk for them and can lead to high cycle fatigue life reduction or even mechanical failure. This aeroelastic instability depends on the interaction between aerodynamics and structural dynamics and it is hard to predict accurately due to its sensitivity to the details during operation. In 2014, as part of the E-Break European Union research project, an experimental campaign aiming to study

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Pinelli, Lorenzo, Michele Marconcini, Roberto Pacciani, Paolo Gaetani, and Giacomo Persico. "Computational and Experimental Study of the Unsteady Convection of Entropy Waves Within a High Pressure Turbine Stage." In ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2020. http://dx.doi.org/10.1115/gt2020-14725.

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Abstract This paper describes the transport and the interaction of pulsating entropy waves generated by combustor burners within a high pressure turbine stage for aeronautical application. Experiments and Computational Fluid Dynamics (CFD) simulations were carried out in the context of the European Research Project RECORD. Experimental campaigns considering burner-representative temperature fluctuations (in terms of spot shape, fluctuation frequency and total temperature variation percentage) injected upstream of an un-cooled high-pressure gas turbine stage have been performed in the high-spee

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Charbonnier, D., P. Ott, M. Jonsson, Th Ko¨bke, and F. Cottier. "Comparison of Numerical Investigations With Measured Heat Transfer Performance of a Film Cooled Turbine Vane." In ASME Turbo Expo 2008: Power for Land, Sea, and Air. ASMEDC, 2008. http://dx.doi.org/10.1115/gt2008-50623.

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Detailed surface measurements of the heat transfer coefficient and the film cooling effectiveness by application of the transient liquid crystal method were carried out on a heavily film cooled nozzle guide vane (NGV) in a linear cascade wind tunnel at the EPFL as part of the European Research Project TATEF2 (Turbine Aero-Thermal External Flows 2). The external cooling setup included a showerhead cooling scheme and suction and pressure side of the airfoil several rows of fan-shaped cooling holes. By testing two different cooling flow rates at a NGV exit Reynolds number of 1.46E+06, detailed ae

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Spyrakos, Constantine, and Charilaos Maniatakis. "SEISMIC PROTECTION OF MONUMENTS AND HISTORIC STRUCTURES – THE SEISMO RESEARCH PROJECT." In VII European Congress on Computational Methods in Applied Sciences and Engineering. Institute of Structural Analysis and Antiseismic Research School of Civil Engineering National Technical University of Athens (NTUA) Greece, 2016. http://dx.doi.org/10.7712/100016.2187.15540.

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Toniolo, G. "SAFECAST PROJECT: EUROPEAN RESEARCH ON SEISMIC BEHAVIOUR OF THE CONNECTIONS OF PRECAST STRUCTURES." In 4th International Conference on Computational Methods in Structural Dynamics and Earthquake Engineering. Institute of Structural Analysis and Antiseismic Research School of Civil Engineering National Technical University of Athens (NTUA) Greece, 2014. http://dx.doi.org/10.7712/120113.4609.c1430.

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Luquet, David, Francois Julienne, Aurélien Arntz, and Eric Lippinois. "Evaluation of the Numerical Modelling of a High Pressure Turbine Test Rig." In ASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2019. http://dx.doi.org/10.1115/gt2019-90483.

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Abstract To improve the fuel efficiency demanded by airlines and regulations, the turbomachinery industry is required to steadily enhance engine performances and numerical prediction capabilities. One of the solutions is the lean burn combustor which dramatically reduces NOx levels compared to rich one. However, one drawback of this technology is its impact on the High-pressure turbine due to large swirl and reduced cooling airflow, inducing large spatial and temporal variations in the turbine inlet condition. This can drastically change the operation of the turbine and our ability to model it

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Parra-Santos, Teresa, José M. Molina Jordá, Gabriel Luna-Sandoval, Mariano Cacho-Perez, and J. Rubén Pérez. "Practical Learning on Computational Fluid Dynamics at Undergraduate Level." In ASME 2016 Fluids Engineering Division Summer Meeting collocated with the ASME 2016 Heat Transfer Summer Conference and the ASME 2016 14th International Conference on Nanochannels, Microchannels, and Minichannels. American Society of Mechanical Engineers, 2016. http://dx.doi.org/10.1115/fedsm2016-7542.

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This work involves a methodology for Mechanical Engineering students to learn Computational Fluid Dynamics playing an active role. Students carry out a fluid mechanics down scaled projects with the steps of sensibility of mesh, convergence of numerical algorithm, validation of turbulence model and description of flow patterns. Furthermore, they develop their critical thought when they identify weak points susceptible for improvement. The offer of benchmark test cases ranges from head loses, driven cavities, swirling flows, to external aerodynamics. Simplifications to the level of undergraduate

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Giovannini, Matteo, Filippo Rubechini, Michele Marconcini, Andrea Arnone, and Francesco Bertini. "Analysis of a LPT Rotor Blade for a Geared Engine: Part I — Aero-Mechanical Design and Validation." In ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2016. http://dx.doi.org/10.1115/gt2016-57746.

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The rotational speed of low pressure turbines (LPT) for geared turbofan applications is significantly increased looking for potential benefit in performance, weight and overall dimensions. As a drawback, the high speed LPT are characterized by critical mechanical constraints due to the large centrifugal stresses in conjunction with the use of lightweight materials. The present activity was carried out in the framework of the Clean Sky European research project ITURB (Optimal High-Lift Turbine Blade Aero-Mechanical Design), aimed at designing and validating a turbine blade for a geared open rot

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Berichte der Organisationen zum Thema "European Computational Aerodynamics Research Project"

García-Espinosa, J., and C. Soriano. Data management plan. Scipedia, 2021. http://dx.doi.org/10.23967/prodphd.2021.9.003.

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This document presents the deliverable D8.1 – the Data Management Plan (DMP) of work package 8 of the prodPhD project. It aims to present the plan for the management, generation, collection, security, preservation and sharing of data generated through the prodPhD project. The DMP is a key element for organizing the project’s data. It provides an analysis of the data, which will be collected, processed and published by the prodPhD consortium. The project embraces the initiatives of the European Commission to promote the open access to research data, aiming to improve and maximize access to and

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