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000130151 001__ 130151 000130151 005__ 20210226113724.0 000130151 0247_ $$2ISSN$$a0169-5983 000130151 0247_ $$2WOS$$aWOS:000260598600003 000130151 0247_ $$2DOI$$a10.1016/j.fluiddyn.2008.02.003 000130151 0247_ $$2HSB$$aalm10089055 000130151 0247_ $$2SCOPUS$$aSCOPUS:2-s2.0-53549112467 000130151 037__ $$aRWTH-CONV-011323 000130151 041__ $$aEnglish 000130151 1001_ $$0P:(DE-82)006349$$aMählmann, Stefan$$b0$$eAuthor 000130151 245__ $$aDisturbance evolution in the leading-edge region of a blunt flat plate in supersonic flow$$honline, print 000130151 260__ $$aAmsterdam [u.a.]$$bElsevier$$c2008 000130151 3367_ $$0PUB:(DE-HGF)16$$2PUB:(DE-HGF)$$aJournal Article$$bjournal$$mjournal 000130151 3367_ $$2DataCite$$aOutput Types/Journal article 000130151 3367_ $$00$$2EndNote$$aJournal Article 000130151 3367_ $$2BibTeX$$aARTICLE 000130151 3367_ $$2ORCID$$aJOURNAL_ARTICLE 000130151 3367_ $$2DRIVER$$aarticle 000130151 591__ $$aGermany 000130151 653_7 $$2eng$$aLeading-edge receptivity 000130151 653_7 $$2eng$$aBoundary-layer instability 000130151 653_7 $$2eng$$aBlunt flat plate 000130151 653_7 $$2eng$$aSupersonic flow 000130151 653_7 $$2eng$$aSpectral methods 000130151 7001_ $$0P:(DE-82)IDM00681$$aSchröder, Wolfgang$$b1$$eAuthor 000130151 773__ $$0PERI:(DE-600)2003039-3$$a10.1016/j.fluiddyn.2008.02.003$$n11/12$$p803-826$$tFluid dynamics research$$v40$$x0169-5983 000130151 909CO $$ooai:publications.rwth-aachen.de:130151$$pVDB 000130151 9151_ $$0StatID:(DE-HGF)0031$$2StatID$$aPeer reviewed article 000130151 9201_ $$0I:(DE-82)415110_20140620$$k415110$$lLehrstuhl für Strömungslehre und Aerodynamisches Institut$$x0 000130151 961__ $$c2014-08-12$$x2008-07-23$$z2012-02-20 000130151 970__ $$aalm10089055 000130151 980__ $$ajournal 000130151 980__ $$aI:(DE-82)415110_20140620 000130151 980__ $$aVDB 000130151 980__ $$aUNRESTRICTED 000130151 980__ $$aConvertedRecord