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Titlebook: Recent Advances in Aerodynamics; Proceedings of an In Anjaneyulu Krothapalli,Charles A. Smith Conference proceedings 1986 Springer-Verlag N

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書目名稱Recent Advances in Aerodynamics
副標(biāo)題Proceedings of an In
編輯Anjaneyulu Krothapalli,Charles A. Smith
視頻videohttp://file.papertrans.cn/823/822594/822594.mp4
圖書封面Titlebook: Recent Advances in Aerodynamics; Proceedings of an In Anjaneyulu Krothapalli,Charles A. Smith Conference proceedings 1986 Springer-Verlag N
描述The Joint Institute for Aeronautics and Acoustics at Stanford University was established in October 1973 to provide an academic environment for long-term cooperative research between Stanford and NASA Ames Research Center. Since its establishment, the In- stitute has wnducted theoretical and experimental work in the areas of aerodynamics, acoustics, fluid mechanics, flight dynamics, guid- ance and control, and human factors. This research has involved Stanford faculty, research associates, graduate students, and many distinguished visitors in collaborative efforts with the research staff of NASA Ames Research Center. The occasion of the Institute‘s tenth anniversary was used to reflect back on where that research has brought us, and to consider where our endeavors should be directed next. Thus, an International Symposium was held to review recent advances in the fields relevant to the activities of the Institute and to discuss the areas of research to be undertaken in the future. This anniversary was also chosen a.."1 an opportunity to honor one of the Institute‘s founders and its di- rector, Professor Krishnamurty Karamcheti. It has been his creative inspiration that has provided
出版日期Conference proceedings 1986
關(guān)鍵詞aerodynamics; dynamics; fluid mechanics; mechanics
版次1
doihttps://doi.org/10.1007/978-1-4612-4972-6
isbn_softcover978-1-4612-9379-8
isbn_ebook978-1-4612-4972-6
copyrightSpringer-Verlag New York Inc. 1986
The information of publication is updating

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Advances in the Understanding and Computation of Unsteady Transonic Flowdisturbances. The second is the effect of wind tunnel walls on unsteady transonic testing. The results that are presented derive from an investigation of unsteady transonic flow initiated at the University of Arizona in 1977, and that have continued there since then. While these studies were launche
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Modeling of Turbulent Separated Flows for Aerodynamic Applications resulting from solutions of the mass-averaged Navier-Stokes equations. Emphasis is placed on bench-mark flows that represent simplified (but realistic) aerodynamic phenomena. These include impinging shock waves, compression corners, glancing shock waves, trailing edge regions, and supersonic high a
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Vortex-Edge Interactionsmber of applications including helicopter rotors, marine propellors, as well as a variety of flap, cavity, tube bundle, and valve/gate configurations. In addition, the interaction of these vorticity fields with the leading-edge provides the initial conditions for evolution of the downstream boundary
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Large-Scale Coherent Structures in Free Turbulent Flows and Their Aerodynamic Sound from conservation principles, including, for instance, the role of fluctuating disturbances on the spreading rate, mode-mode interactions, the growth and decay of coherent structures and their negative production rate and energy exchanges between the various scales of motion. This sets the stage fo
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