000 03126nam a22005295i 4500
001 978-3-662-44365-1
003 DE-He213
005 20200420220223.0
007 cr nn 008mamaa
008 140828s2015 gw | s |||| 0|eng d
020 _a9783662443651
_9978-3-662-44365-1
024 7 _a10.1007/978-3-662-44365-1
_2doi
050 4 _aTA357-359
072 7 _aTGMF
_2bicssc
072 7 _aTGMF1
_2bicssc
072 7 _aTEC009070
_2bisacsh
072 7 _aSCI085000
_2bisacsh
082 0 4 _a620.1064
_223
100 1 _aWang, Zhi-Hui.
_eauthor.
245 1 0 _aTheoretical Modelling of Aeroheating on Sharpened Noses Under Rarefied Gas Effects and Nonequilibrium Real Gas Effects
_h[electronic resource] /
_cby Zhi-Hui Wang.
264 1 _aBerlin, Heidelberg :
_bSpringer Berlin Heidelberg :
_bImprint: Springer,
_c2015.
300 _aXV, 94 p. 46 illus., 27 illus. in color.
_bonline resource.
336 _atext
_btxt
_2rdacontent
337 _acomputer
_bc
_2rdamedia
338 _aonline resource
_bcr
_2rdacarrier
347 _atext file
_bPDF
_2rda
490 1 _aSpringer Theses, Recognizing Outstanding Ph.D. Research,
_x2190-5053
505 0 _aIntroduction -- Theoretical Modeling of Aeroheating under Rarefied Gas Effects -- Theoretical modeling of the chemical nonequilibrium flow behind a normal shock wave -- Theoretical modeling of aero-heating under nonequilibrium real gas effects -- Conclusions and prospect.
520 _aTheoretical Modelling of Aeroheating on Sharpened Noses under Rarefied Gas Effects and Nonequilibrium Real Gas Effects employs a theoretical modeling method to study hypersonic flows and aeroheating on sharpened noses under rarefied gas effects and nonequilibrium real gas effects that are beyond the scope of traditional fluid mechanics. It reveals the nonlinear and nonequilibrium features, discusses the corresponding flow and heat transfer mechanisms, and ultimately establishes an analytical engineering theory framework for hypersonic rarefied and chemical nonequilibrium flows. The original analytical findings presented are not only of great academic significance, but also hold considerable potential for applications in engineering practice. The study explores a viable new approach, beyond the heavily relied-upon numerical methods and empirical formulas, to the present research field, which could be regarded as a successful implementation of the idea and methodology of the engineering sciences.
650 0 _aEngineering.
650 0 _aFluids.
650 0 _aFluid mechanics.
650 0 _aAerospace engineering.
650 0 _aAstronautics.
650 1 4 _aEngineering.
650 2 4 _aEngineering Fluid Dynamics.
650 2 4 _aFluid- and Aerodynamics.
650 2 4 _aAerospace Technology and Astronautics.
710 2 _aSpringerLink (Online service)
773 0 _tSpringer eBooks
776 0 8 _iPrinted edition:
_z9783662443644
830 0 _aSpringer Theses, Recognizing Outstanding Ph.D. Research,
_x2190-5053
856 4 0 _uhttp://dx.doi.org/10.1007/978-3-662-44365-1
912 _aZDB-2-ENG
942 _cEBK
999 _c52036
_d52036