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008			171103s2018 gw | s |||| 0|eng d
020			_a9783319678528
024	7		_a10.1007/978-3-319-67852-8 _2doi
040			_bspa _cES-MaUEC _dES-MaUEC
050		4	_aUG1242.D7 _bK365 2018 EB
100	1		_aKanistras, Konstantinos. _eautor. _4aut _4http://id.loc.gov/vocabulary/relators/aut
245	1	0	_aFoundations of Circulation Control Based Small-Scale Unmanned Aircraft _bA Comprehensive Methodology from Concept to Design and Experimental Testing _cby Konstantinos Kanistras, Kimon P. Valavanis, Matthew J. Rutherford.
264		1	_aCham _bSpringer International Publishing _c2018
300			_a1 recurso en línea (XVII, 138 páginas 93 ilustraciones, 85 ilustraciones a color.)
336			_2rdacontent _aTexto _btxt
337			_2rdamedia _aelectrónico _bc
338			_2rdacarrier _arecurso electrónico _bcr
347			_atext file _bPDF
490	0		_aIntelligent Systems, Control and Automation: Science and Engineering, _x2213-8986 _v91
490	0		_aEngineering (Springer-11647)
505	0		_aIntroduction -- The History of Circulation Control -- Fundamentals of Circulation Control -- Model Description -- Plenum Design -- Wind Tunnel & Instrumentation -- Wind Tunnel Results & Discussion -- UC2AV: Unmanned Circulation Control Aerial Vehicle -- Air Supply Unit (ASU) -- Takeoff Performance & Instrumentation -- Flight Testing -- Epilogue.
520	3		_aThis book focuses on using and implementing Circulation Control (CC) - an active flow control method used to produce increased lift over the traditionally used systems, like flaps, slats, etc. - to design a new type of fixed-wing unmanned aircraft that are endowed with improved aerodynamic efficiency, enhanced endurance, increased useful payload (fuel capacity, battery cells, on-board sensors) during cruise flight, delayed stall, and reduced runway during takeoff and landing. It presents the foundations of a step-by-step comprehensive methodology from design to implementation and experimental testing of Coandǎ based Circulation Control Wings (CCWs) and CC system, both integral components of the new type of aircraft, called Unmanned Circulation Control Air Vehicle. The methodology is composed of seven coupled phases: theoretical and mathematical analysis, design, simulation, 3-D printing/prototyping, wind tunnel testing, wing implementation and integration, and flight testing. The theoretical analysis focuses on understanding the physics of the flow and on defining the design parameters of the geometry restrictions of the wing and the plenum. The design phase centers on: designs of Coandǎ surfaces based on wing geometry specifications; designing and modifying airfoils from well-known ones (NACA series, Clark-Y, etc.); plenum designs for flow uniformity; dual radius flap designs to delay flow separation and reduce cruise drag. The simulation phase focuses on Computational Fluid Dynamics (CFD) analysis and simulations, and on calculating lift and drag coefficients of the designed CCWs in a simulation environment. 3-D printing and prototyping focuses on the actual construction of the CCWs. Wind tunnel testing centers on experimental studies in a laboratory environment. One step before flight testing is implementation of the qualified CCW and integration on the UAV platform, along with the CC system. Flight testing is the final phase, where design validation is performed. This book is the first of its kind, and it is suitable for students and researchers interested in the design and development of CCWs for small-scale aircraft. Background knowledge on fundamental Aerodynamics is required.   .
988			_aEBSPRINGER_2018
650		7	_2embne _9667210 _aDrones
700	1		_aValavanis, Kimon P. _eautor. _4aut _4http://id.loc.gov/vocabulary/relators/aut _1http://viaf.org/viaf/29620830/
700	1		_aRutherford, Matthew J. _eautor. _4aut _4http://id.loc.gov/vocabulary/relators/aut
776	0	8	_iEdición impresa: _z9783319678511
776	0	8	_iEdición impresa: _z9783319678535
776	0	8	_iEdición impresa: _z9783319884967
856	4	0	_uhttps://go.openathens.net/redirector/universidadeuropea.es?url=https://doi.org/10.1007/978-3-319-67852-8 _zAcceso a este recurso digital (usuarios Universidad Europea de Madrid)
942			_2lcc _cLE