{"71763":{"#nid":"71763","#data":{"type":"event","title":"AE Distinguished Lecture Series","body":[{"value":"\u003Cp align=\u0022center\u0022\u003EAE Distinguished Lecture Series Presents\u003C\/p\u003E\u003Cp align=\u0022center\u0022\u003EMODEL ORDER REDUCTION FOR TIME-CRITICAL APPLICATIONS IN AERONAUTICAL ENGINEERING\u003C\/p\u003E\u003Cp align=\u0022center\u0022\u003ECharbel Farhat\u003C\/p\u003E\u003Cp align=\u0022center\u0022\u003EDepartment of Aeronautics \u0026amp; Astronautics\u003C\/p\u003E\u003Cp align=\u0022center\u0022\u003EStanford University, Stanford, CA USA\u003C\/p\u003E\u003Cp align=\u0022center\u0022\u003EThursday, October 27, 2011 @ 4:00pm \u003C\/p\u003E\u003Cp align=\u0022center\u0022\u003EMontgomery Knight (G442)\u003C\/p\u003E\u003Cp\u003EAbstract:\u003Cbr \/\u003EIn many applications, high-fidelity time-dependent numerical simulations remain so computationally intensive that they cannot be used as often as needed, or are more often used in special circumstances than routinely. This is the case, for example, for turbulent CFD computations at high Reynolds numbers. Consequently, in many engineering fields including aeronautics, the impact of computational sciences on time-critical operations such as design, design optimization, control, and flight test has not yet fully materialized. For these operations, reduced order models that can faithfully reproduce the essential features of the larger computational models at a fraction of their computational cost offer a promising alternative. This presentation will cover recent advances in this field. It will also demonstrate real-time performance on mobile devices of a CFD-based computational methodology for assisting flutter flight-testing and the aerodynamic design of a Formula 1 car.\u003C\/p\u003E\u003Cp\u003EBIO:\u003Cbr \/\u003ECharbel Farhat is the Vivian Church Hoff Professor of Aircraft Structures, Chairman of the Department of Aeronautics and Astronautics, and Director of the Army High Performance Computing Research Center at Stanford University. He is designated as an ISI Highly Cited Author in Engineering by the Institute for Science Information (ISI) Web of Knowledge, Thomson Scientific Company. He was knighted by the French Government in the Order of Academic Palms and awarded the Medal of Chevalier dans l\u2019Ordre des Palmes Academiques. He is also the recipient of several other academic distinctions including the Lifetime Achievement Award from ASME, the Structures, Structural Dynamics and Materials Award from AIAA, the John von Neumann Medal, Computational and Applied Sciences Award, and R. H. Gallagher Special Achievement Award from USACM, the Gordon Bell Prize and Sidney Fernbach Award from IEEE, the Computational Mechanics Award from IACM, and the Modeling and Simulation Award from the Department of Defense. Professor Farhat is a Fellow of AIAA, ASME, USACM, IACM, SIAM, and WIF. His research interests include nonlinear aeroelastic phenomena for modern fighter jets, micro aerial vehicles, aeroacoustics, fluid-structure interaction, underwater acoustic scattering, underwater implosion, shape optimization, multi-scale modeling, model order reduction, and real-time computing.\u003C\/p\u003E","summary":null,"format":"limited_html"}],"field_subtitle":"","field_summary":[{"value":"\u003Cp align=\u0022center\u0022\u003EAE Distinguished Lecture Series Presents\u003C\/p\u003E\u003Cp align=\u0022center\u0022\u003EMODEL ORDER REDUCTION FOR TIME-CRITICAL APPLICATIONS IN AERONAUTICAL ENGINEERING\u003C\/p\u003E\u003Cp align=\u0022center\u0022\u003ECharbel Farhat\u003C\/p\u003E\u003Cp align=\u0022center\u0022\u003EDepartment of Aeronautics \u0026amp; Astronautics\u003C\/p\u003E\u003Cp align=\u0022center\u0022\u003EStanford University, Stanford, CA USA\u003C\/p\u003E\u003Cp align=\u0022center\u0022\u003EThursday, October 27, 2011 @ 4:00pm \u2013 Montgomery Knight - G442\u003C\/p\u003E\u003Cp\u003EAbstract:\u003Cbr \/\u003EIn many applications, high-fidelity time-dependent numerical simulations remain so computationally intensive that they cannot be used as often as needed, or are more often used in special circumstances than routinely. This is the case, for example, for turbulent CFD computations at high Reynolds numbers. Consequently, in many engineering fields including aeronautics, the impact of computational sciences on time-critical operations such as design, design optimization, control, and flight test has not yet fully materialized. For these operations, reduced order models that can faithfully reproduce the essential features of the larger computational models at a fraction of their computational cost offer a promising alternative. This presentation will cover recent advances in this field. It will also demonstrate real-time performance on mobile devices of a CFD-based computational methodology for assisting flutter flight-testing and the aerodynamic design of a Formula 1 car.\u003C\/p\u003E\u003Cp\u003EBIO:\u003Cbr \/\u003ECharbel Farhat is the Vivian Church Hoff Professor of Aircraft Structures, Chairman of the Department of Aeronautics and Astronautics, and Director of the Army High Performance Computing Research Center at Stanford University. He is designated as an ISI Highly Cited Author in Engineering by the Institute for Science Information (ISI) Web of Knowledge, Thomson Scientific Company. He was knighted by the French Government in the Order of Academic Palms and awarded the Medal of Chevalier dans l\u2019Ordre des Palmes Academiques. He is also the recipient of several other academic distinctions including the Lifetime Achievement Award from ASME, the Structures, Structural Dynamics and Materials Award from AIAA, the John von Neumann Medal, Computational and Applied Sciences Award, and R. H. Gallagher Special Achievement Award from USACM, the Gordon Bell Prize and Sidney Fernbach Award from IEEE, the Computational Mechanics Award from IACM, and the Modeling and Simulation Award from the Department of Defense. Professor Farhat is a Fellow of AIAA, ASME, USACM, IACM, SIAM, and WIF. His research interests include nonlinear aeroelastic phenomena for modern fighter jets, micro aerial vehicles, aeroacoustics, fluid-structure interaction, underwater acoustic scattering, underwater implosion, shape optimization, multi-scale modeling, model order reduction, and real-time computing.\u003C\/p\u003E","format":"limited_html"}],"field_summary_sentence":[{"value":"Aerospace Engineering is proud to present Professor Charbel Farhat, Department of Aeronautics \u0026 Astronautics, Stanford University, Stanford, CA"}],"uid":"27516","created_gmt":"2011-10-24 13:40:04","changed_gmt":"2016-10-08 01:56:28","author":"Glenda Duncan","boilerplate_text":"","field_publication":"","field_article_url":"","field_event_time":{"event_time_start":"2011-10-27T17:00:00-04:00","event_time_end":"2011-10-27T18:00:00-04:00","event_time_end_last":"2011-10-27T18:00:00-04:00","gmt_time_start":"2011-10-27 21:00:00","gmt_time_end":"2011-10-27 22:00:00","gmt_time_end_last":"2011-10-27 22:00:00","rrule":null,"timezone":"America\/New_York"},"extras":[],"groups":[{"id":"1239","name":"School of Aerospace Engineering"}],"categories":[],"keywords":[{"id":"10010","name":"aeronautical engineering"}],"core_research_areas":[],"news_room_topics":[],"event_categories":[{"id":"1795","name":"Seminar\/Lecture\/Colloquium"}],"invited_audience":[],"affiliations":[],"classification":[],"areas_of_expertise":[],"news_and_recent_appearances":[],"phone":[],"contact":[{"value":"\u003Cp\u003EGlenda Duncan (404)894-3032\u003C\/p\u003E","format":"limited_html"}],"email":[],"slides":[],"orientation":[],"userdata":""}}}