000921350 000__ 03858cam\a2200529Ii\4500 000921350 001__ 921350 000921350 005__ 20230306150714.0 000921350 006__ m\\\\\o\\d\\\\\\\\ 000921350 007__ cr\nn\nnnunnun 000921350 008__ 191202s2019\\\\gw\a\\\\o\\\\\000\0\eng\d 000921350 019__ $$a1129792185 000921350 020__ $$a9783030332532 000921350 020__ $$a3030332535 000921350 020__ $$z9783030332525 000921350 020__ $$z3030332527 000921350 0247_ $$a10.1007/978-3-030-33253-2$$2doi 000921350 035__ $$aSP(OCoLC)on1134694052 000921350 035__ $$aSP(OCoLC)1134694052$$z(OCoLC)1129792185 000921350 040__ $$aUPM$$beng$$cUPM$$dGW5XE$$dYDX 000921350 049__ $$aISEA 000921350 050_4 $$aTA357 000921350 050_4 $$aTA342-343 000921350 08204 $$a003.3$$223 000921350 1001_ $$aPontes, José.$$eauthor. 000921350 24513 $$aAn introduction to compressible flows with applications :$$bQuasi-One-Dimensional Approximation and General Formulation for Subsonic, Transonic and Supersonic Flows /$$cJosé Pontes, Norberto Mangiavacchi, Gustavo R. Anjos. 000921350 264_1 $$aCham :$$bSpringer,$$c2019. 000921350 300__ $$a1 online resource (ix, 129 pages) :$$billustrations 000921350 336__ $$atext$$btxt$$2rdacontent 000921350 337__ $$acomputer$$bc$$2rdamedia 000921350 338__ $$aonline resource$$bcr$$2rdacarrier 000921350 347__ $$atext file$$bPDF$$2rda 000921350 4901_ $$aSpringerBriefs in Mathematics,$$x2191-8198 000921350 5050_ $$aPreface -- Compressible Potential Flows -- One-dimensional Compressible Flows -- Oblique Shocks -- Uniform Flows with Small Perturbations -- The Basic Equations of Compressible Fluid Flow. 000921350 506__ $$aAccess limited to authorized users. 000921350 520__ $$aThis book offers a concise and practical survey of the principles governing compressible flows, along with selected applications. It starts with derivation of the time-dependent, three-dimensional equation of compressible potential flows, and a study of weak waves, including evaluation of the sound speed in gases. The following chapter addresses quasi-one-dimensional flows, the study of normal shock waves, and flow in ducts with constant cross section subjected to friction and/or heat transfer. It also investigates the effects of friction and heat transfer in ducts with variable cross section. The chapter ends by pointing to the analogy between one-dimensional compressible flows and open channel hydraulics. Further, the book discusses supersonic flows, including the study of oblique shock waves, and supersonic flows over corners and wedges. It also examines Riemann problems, numerical resolution of the wave equation, and of nonlinear hyperbolic problems, including propagation of strong waves. A subsequent chapter focuses on the small perturbation theory of subsonic, transonic and supersonic flows around slender bodies aligned or almost aligned to the uniform inflow. In particular, it explores subsonic and supersonic flows over a wavy wall. Lastly, an appendix with a short derivation of the Fluid Mechanics basic equations is included. The final chapter addresses the problem of transonic flows where both subsonic and supersonic are present. Lastly, an appendix with a short derivation of the Fluid Mechanics basic equations is included. Illustrated with several practical examples, this book is a valuable tool to understand the most fundamental mathematical principles of compressible flows. Graduate Mathematics, Physics and Engineering students as well as researchers with an interest in the aerospace sciences benefit from this work. 000921350 650_0 $$aFluid mechanics. 000921350 650_0 $$aFluids. 000921350 650_0 $$aCompressibility. 000921350 650_0 $$aMathematical models. 000921350 7001_ $$aMangiavacchi, Norberto.$$eauthor. 000921350 7001_ $$aAnjos, Gustavo R.$$eauthor. 000921350 77608 $$iPrint version: $$z9783030332525 000921350 830_0 $$aSpringerBriefs in mathematics. 000921350 852__ $$bebk 000921350 85640 $$3SpringerLink$$uhttps://univsouthin.idm.oclc.org/login?url=http://link.springer.com/10.1007/978-3-030-33253-2$$zOnline Access$$91397441.1 000921350 909CO $$ooai:library.usi.edu:921350$$pGLOBAL_SET 000921350 980__ $$aEBOOK 000921350 980__ $$aBIB 000921350 982__ $$aEbook 000921350 983__ $$aOnline 000921350 994__ $$a92$$bISE