LEADER 04127nam 2200685 a 450 001 9911006561403321 005 20200520144314.0 010 $a1-139-12397-1 010 $a1-283-29826-0 010 $a1-139-12199-5 010 $a9786613298263 010 $a0-511-84275-9 010 $a1-139-11625-8 010 $a1-139-12691-1 010 $a1-139-10972-3 010 $a1-139-11189-2 010 $a1-139-11408-5 035 $a(CKB)2550000000056577 035 $a(EBL)775006 035 $a(SSID)ssj0000555493 035 $a(PQKBManifestationID)11343703 035 $a(PQKBTitleCode)TC0000555493 035 $a(PQKBWorkID)10518866 035 $a(PQKB)10950431 035 $a(UkCbUP)CR9780511842757 035 $a(MiAaPQ)EBC775006 035 $a(PPN)261348469 035 $a(EXLCZ)992550000000056577 100 $a20110114d2011 uy 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 00$aShock wave-boundary-layer interactions /$fedited by Holger Babinsky, John K. Harvey 210 $aCambridge ;$aNew York $cCambridge University Press$d2011 215 $a1 online resource (xvii, 461 pages) $cdigital, PDF file(s) 225 1 $aCambridge aerospace series 300 $aTitle from publisher's bibliographic system (viewed on 05 Oct 2015). 311 $a1-107-64653-7 311 $a0-521-84852-0 320 $aIncludes bibliographical references and index. 327 $aMachine generated contents note: 1. Introduction John K. Harvey and Holger Babinsky; 2. Physical introduction Jean Delery; 3. Transonic shock wave boundary layer interactions Holger Babinsky and Jean Delery; 4. Ideal gas shock wave turbulent boundary layer interactions in supersonic flows and their modeling - two dimensional interactions Alexander A. Zheltovodov and Doyle D. Knight; 5. Ideal gas shock wave turbulent boundary layer interactions in supersonic flows and their modeling - three dimensional interactions Doyle D. Knight and Alexander A. Zheltovodov; 6. Experimental studies of shock wave/boundary layer interactions in hypersonic flows Michael S. Holden; 7. Numerical simulation of hypersonic shock wave boundary layer interactions Graham V. Candler; 8. Shock wave/boundary layer interactions taking place in hypersonic flows John K. Harvey; 9. Shock wave unsteadiness in turbulent shock wave boundary layer interactions P. Dupont, J.F Debieve, and J.P Dussauge; 10. Analytical treatment of shock/boundary layer interactions George Inger. 330 $a"Shock Wave/Boundary Layer Interaction (SBLI) is a fundamental phenomenon in gas dynamics and frequently a defining feature in high speed aerodynamic flowfields. The interactions can be found in practical situations, ranging from transonic aircraft wings to hypersonic vehicles and engines. SBLI's have the potential to pose serious problems and is thus a critical issue for aerospace applications. This is the first book devoted solely to a comprehensive, state of the art explanation of the phenomenon with coverage of all flow regimes where SBLI's occur. The book includes contributions from leading international experts who share their insight into SBLI physics and the impact of these interactions on practical flow situations. This book is aimed at practitioners and graduate students in aerodynamics who wish to familiarise themselves with all aspects of SBLI flows. It is a valuable resource for the specialist because it gathers experimental, computational and theoretical knowledge in one place"--$cProvided by publisher. 410 0$aCambridge aerospace series. 606 $aShock waves 606 $aBoundary layer 615 0$aShock waves. 615 0$aBoundary layer. 676 $a629.132/37 686 $aTEC009000$2bisacsh 701 $aBabinsky$b Holger$01825402 701 $aHarvey$b John$g(John K.)$037852 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9911006561403321 996 $aShock wave-boundary-layer interactions$94393021 997 $aUNINA