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Titlebook: Design and Development of Aerospace Vehicles and Propulsion Systems; Proceedings of SAROD S. Kishore Kumar,Indira Narayanaswamy,V. Ramesh C

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书目名称Design and Development of Aerospace Vehicles and Propulsion Systems
副标题Proceedings of SAROD
编辑S. Kishore Kumar,Indira Narayanaswamy,V. Ramesh
视频video
概述Covers aerodynamics of aerospace vehicles.Special focus on Stealth in Aerospace Design.Looks at all aspects vehicle and propulsion system design
丛书名称Lecture Notes in Mechanical Engineering
图书封面Titlebook: Design and Development of Aerospace Vehicles and Propulsion Systems; Proceedings of SAROD S. Kishore Kumar,Indira Narayanaswamy,V. Ramesh C
描述This book presents selected papers presented in the Symposium on Applied Aerodynamics and Design of Aerospace Vehicles (SAROD 2018), which was  jointly organized  by Aeronautical Development Agency (the nodal agency for the design and development of combat aircraft in India),  Gas-Turbine Research Establishment (responsible for design and development of gas turbine engines for military applications), and CSIR-National Aerospace Laboratories (involved in major aerospace programs in the country such as SARAS program, LCA, Space Launch Vehicles, Missiles and UAVs). It brings together experiences of aerodynamicists in India as well as abroad in Aerospace Vehicle Design, Gas Turbine Engines, Missiles and related areas. It is a useful volume for researchers, professionals and students interested in diversified areas of aerospace engineering.
出版日期Conference proceedings 2021
关键词Aerodynamics of Aerospace Vehicles; Conceptual Design of Aircraft; Turbomachinery Flows; Intake Aerodyn
版次1
doihttps://doi.org/10.1007/978-981-15-9601-8
isbn_softcover978-981-15-9603-2
isbn_ebook978-981-15-9601-8Series ISSN 2195-4356 Series E-ISSN 2195-4364
issn_series 2195-4356
copyrightSpringer Nature Singapore Pte Ltd. 2021
The information of publication is updating

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Wechselspannung und Wechselstrom, been advantageous in the study of aero-elastic behavior of lifting surfaces. Preliminary design of an UAV requires detailed understanding of aerodynamic and structural operational boundaries; to arrive at an optimal wing. High aspect ratio wings are being employed in Medium Altitude Long Endurance
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,Feldeffekttransistor, MOSFET und Röhren,tion for the study arises from aeroelastic studies of turbomachinery blades, where the unsteady forces acting on a blade due to different sources is examined. In order to identify the root cause of the various phenomena affecting the aeroelastic stability, it is necessary to observe the effect of on
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https://doi.org/10.1007/978-3-658-07874-4ltered external flow contributes to an additional force on the vehicle in addition to the jet thrust thereby effecting its performance. In this study, numerical simulations were carried out to estimate the effect of injection location and body attitude on the overall performance of a Reaction Contro
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Ermittlung von Zinsstrukturkurven retaining the same gap and aspect ratio to explicitly decipher the role of chord on grid fin aerodynamics through numerical analysis. Solver validation is followed by comprehensive examination of the pertinent aerodynamic coefficient results associated with different grid fin chord variants. The st
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