000			05382nam a22006375i 4500
999			_c13112 _d13112
001			978-3-319-67852-8
003			DE-He213
005			20211207094414.0
008			171103s2018 gw | s |||| 0|eng d
020			_a9783319678528
040			_cAIKTC-KRRC
041			_aENG
072		7	_aTRP _2bicssc
072		7	_aTEC002000 _2bisacsh
072		7	_aTRP _2thema
072		7	_aTTDS _2thema
082	0	4	_a629.1 _223
100	1		_aKanistras, Konstantinos. _eauthor. _4aut _4http://id.loc.gov/vocabulary/relators/aut
245	1	0	_aFoundations of Circulation Control Based Small-Scale Unmanned Aircraft _h[electronic resource] : _bA Comprehensive Methodology from Concept to Design and Experimental Testing /
250			_a1st ed. 2018.
264		1	_aCham : _bSpringer International Publishing : _bImprint: Springer, _c2018.
300			_aXVII, 138 p. 93 illus., 85 illus. in color. _bCard Paper
336			_atext _btxt _2rdacontent
337			_acomputer _bc _2rdamedia
338			_aonline resource _bcr _2rdacarrier
347			_atext file _bPDF _2rda
490	1		_aIntelligent Systems, Control and Automation: Science and Engineering, _x2213-8986 ; _v91
520			_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.   .
650		0	_aMechanical Engineering _94626
653			_aAerospace Technology and Astronautics.
653			_aControl, Robotics, Mechatronics.
653			_aFluid- and Aerodynamics.
653			_aEngineering Fluid Dynamics.
700	1		_aValavanis, Kimon P. _eauthor. _4aut _4http://id.loc.gov/vocabulary/relators/aut
700	1		_aRutherford, Matthew J. _eauthor. _4aut _4http://id.loc.gov/vocabulary/relators/aut
710	2		_aSpringerLink (Online service)
773	0		_tSpringer Nature eBook
776	0	8	_iPrinted edition: _z9783319678511
776	0	8	_iPrinted edition: _z9783319678535
776	0	8	_iPrinted edition: _z9783319884967
830		0	_aIntelligent Systems, Control and Automation: Science and Engineering, _x2213-8986 ; _v91
856	4	0	_uhttps://doi.org/10.1007/978-3-319-67852-8 _zClick here to access eBook in Springer Nature platform. (Within Campus only.)
942			_cEBOOKS _2ddc