LEADER 01116nam--2200373---4500 001 990000688100203316 005 20060331140825.0 035 $a0068810 035 $aUSA010068810 035 $a(ALEPH)000068810USA01 035 $a0068810 100 $a20011015d1971----km-y0ENGy0103----ba 101 $aita 102 $aIT 200 1 $a<> Dalida$fL. Groto$ga cura di M. Cataudella 210 $aSalerno$cBeta$dc1971 215 $a214 p.$d21 cm 225 2 $aCollana umanistica$iTesti e saggi$v2 410 $12001$aCollana umanistica$iTesti e saggi$v2 676 $a852.4 700 1$aGROTO,$bLuigi$079596 702 1$aCAUTADELLA,$bMichele 801 0$aIT$bsalbc$gISBD 912 $a990000688100203316 951 $aVI.3.A. 1115(V C COLL. 118/2)$b94321 LM$cV C COLL. 951 $aVI.3.A. 1115a(V C COLL. 118/2BIS)$b94322 LM$cV C COLL. 959 $aBK 969 $aUMA 979 $aPATTY$b90$c20011015$lUSA01$h2322 979 $c20020403$lUSA01$h1718 979 $aPATRY$b90$c20040406$lUSA01$h1647 979 $aCOPAT7$b90$c20060331$lUSA01$h1408 996 $aDalida$9960636 997 $aUNISA LEADER 03494nam 22005775 450 001 9910337645303321 005 20200703105722.0 010 $a3-030-02565-9 024 7 $a10.1007/978-3-030-02565-6 035 $a(CKB)4100000007223579 035 $a(MiAaPQ)EBC5615427 035 $a(DE-He213)978-3-030-02565-6 035 $a(PPN)232964378 035 $a(EXLCZ)994100000007223579 100 $a20181213d2019 u| 0 101 0 $aeng 135 $aurcnu|||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aIntroduction to Simple Shock Waves in Air $eWith Numerical Solutions Using Artificial Viscosity /$fby Seán Prunty 205 $a1st ed. 2019. 210 1$aCham :$cSpringer International Publishing :$cImprint: Springer,$d2019. 215 $a1 online resource (257 pages) 225 1 $aShock Wave and High Pressure Phenomena,$x2197-9529 311 $a3-030-02564-0 327 $aBrief outline of the equations of fluid flow -- Waves of finite amplitude -- Conditions across the shock: the Rankine-Hugoniot equations -- Numerical treatment of plane shocks -- Spherical shock waves: the self-similar solution -- Numerical treatment of spherical shock waves. 330 $aThis book provides an elementary introduction to some one-dimensional fluid flow problems involving shock waves in air. The differential equations of fluid flow are approximated by finite difference equations and these in turn are numerically integrated in a stepwise manner. Artificial viscosity is introduced into the numerical calculations in order to deal with shocks. The presentation is restricted to the finite-difference approach to solve the coupled differential equations of fluid flow as distinct from finite-volume or finite-element methods. This text presents the results arising from the numerical solution using Mathcad programming. Both plane and spherical shock waves are discussed with particular emphasis on very strong explosive shocks in air. This text will appeal to students, researchers, and professionals in shock wave research and related fields. Students in particular will appreciate the benefits of numerical methods in fluid mechanics and the level of presentation. 410 0$aShock Wave and High Pressure Phenomena,$x2197-9529 606 $aFluid mechanics 606 $aFluids 606 $aMathematical physics 606 $aPhysics 606 $aEngineering Fluid Dynamics$3https://scigraph.springernature.com/ontologies/product-market-codes/T15044 606 $aFluid- and Aerodynamics$3https://scigraph.springernature.com/ontologies/product-market-codes/P21026 606 $aMathematical Applications in the Physical Sciences$3https://scigraph.springernature.com/ontologies/product-market-codes/M13120 606 $aMathematical Methods in Physics$3https://scigraph.springernature.com/ontologies/product-market-codes/P19013 615 0$aFluid mechanics. 615 0$aFluids. 615 0$aMathematical physics. 615 0$aPhysics. 615 14$aEngineering Fluid Dynamics. 615 24$aFluid- and Aerodynamics. 615 24$aMathematical Applications in the Physical Sciences. 615 24$aMathematical Methods in Physics. 676 $a533.293 700 $aPrunty$b Seán$4aut$4http://id.loc.gov/vocabulary/relators/aut$0999580 906 $aBOOK 912 $a9910337645303321 996 $aIntroduction to Simple Shock Waves in Air$92294351 997 $aUNINA