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020 _a9789401797474
024 7 _a10.1007/978-94-017-9747-4
_2doi
040 _bspa
_dES-MaUEC
050 4 _aTL571
_b2015 EB
100 1 _aVos, Roelof.
_eautor
_4aut
_4http://id.loc.gov/vocabulary/relators/aut
_0http://id.loc.gov/authorities/names/nb2015009159
_1http://viaf.org/viaf/51994296/
245 1 0 _aIntroduction to Transonic Aerodynamics
_cby Roelof Vos, Saeed Farokhi.
264 1 _aDordrecht
_bSpringer International Publishing
_c2015
300 _a1 recurso en línea (XIII, 555 páginas 407 ilustraciones, 15 ilustraciones a color.)
336 _2rdacontent
_aTexto (visual)
_btxt
337 _2rdamedia
_aelectrónico
_bc
338 _2rdacarrier
_arecurso electrónico
_bcr
490 0 _aFluid Mechanics and Its Applications,
_x0926-5112 ;
_v110
490 0 _aEngineering (Springer-11647)
505 0 _a1 Introduction and Historic Perspective -- 2 Review of Fundamental Equations -- 3 Transonic Similarity Laws -- 4 Shock-Expansion Theory -- 5 Method of Characteristics -- 6 Aerodynamics of Non lifting Bodies -- 7 Airfoil Aerodynamics -- 8 Aerodynamics of Swept Wings -- A Isentropic Flow Table -- B Normal Shock Table -- C Prandtl-Meyer Function -- Partial Answers to Selected Problems -- Glossary -- Index.
520 3 _aWritten to teach students the nature of transonic flow and its mathematical foundation, this book offers a much-needed introduction to transonic aerodynamics. The authors present a quantitative and qualitative assessment of subsonic, supersonic, and transonic flow around bodies in two and three dimensions. The book reviews the governing equations and explores their applications and limitations as employed in modeling and computational fluid dynamics.  Some concepts, such as shock and expansion theory, are examined from a numerical perspective. Others, including shock-boundary-layer interaction, are discussed from a qualitative point of view. The book includes 60 examples and more than 200 practice problems. The authors also offer analytical methods such as Method of Characteristics (MOC) that allow readers to practice with the subject matter.  The result is a wealth of insight into transonic flow phenomena and their impact on aircraft design, including compressibility effects, shock and expansion waves, shock-boundary-layer interaction and aeroelasticity.
988 _aEBSPRINGER_2018
650 7 _2embne
_9668900
_aAerodinámica supersónica
700 1 _aFarokhi, Saeed.
_eautor
_4aut
_4http://id.loc.gov/vocabulary/relators/aut
_0http://id.loc.gov/authorities/names/n2007049517
_1http://viaf.org/viaf/38827283/
776 0 8 _iEdición impresa:
_z9789401797467
776 0 8 _iEdición impresa:
_z9789401797481
776 0 8 _iEdición impresa:
_z9789401777698
856 4 0 _uhttps://go.openathens.net/redirector/universidadeuropea.es?url=https://doi.org/10.1007/978-94-017-9747-4
_zAcceso a este recurso digital (usuarios Universidad Europea de Madrid)
942 _2lcc
_cLE
998 _b05/2019
_dz
_ejf
_zSI