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000190318 001__ 190318
000190318 005__ 20231215082833.0
000190318 0247_ $$2ISSN$$a0021-8669
000190318 0247_ $$2ISSN$$a1533-3868
000190318 0247_ $$2WOS$$aWOS:000244136500024
000190318 0247_ $$2DOI$$a10.2514/1.23057
000190318 0247_ $$2HSB$$a999910181048
000190318 0247_ $$2SCOPUS$$aSCOPUS:2-s2.0-33847761088
000190318 037__ $$aRWTH-CONV-066325
000190318 041__ $$aEnglish
000190318 1001_ $$0P:(DE-82)018228$$aWinnemöller, Tobias$$b0$$eAuthor
000190318 1112_ $$aAIAA 44th Aerospace Sciences Meeting and Exhibit$$cReno$$d2006-01-09 - 2006-01-12$$wUSA
000190318 245__ $$aDesign and numerical optimization of thick airfoils including blunt trailing edges$$honline, print
000190318 260__ $$aReston, Va. [u.a.]$$bAmerican Institute of Aeronautics and Astronautics$$c2007
000190318 3367_ $$0PUB:(DE-HGF)16$$2PUB:(DE-HGF)$$aJournal Article$$bjournal$$mjournal
000190318 3367_ $$0PUB:(DE-HGF)8$$2PUB:(DE-HGF)$$aContribution to a conference proceedings
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000190318 591__ $$aGermany
000190318 591__ $$aUSA
000190318 7001_ $$0P:(DE-82)148337$$avan Dam, C. P.$$b1$$eAuthor
000190318 770__ $$a[AIAA 44th Aerospace Sciences Meeting and Exhibit, JAN 09-12, 2006, Reno, NV]
000190318 773__ $$0PERI:(DE-600)2025892-6$$a10.2514/1.23057$$n1$$p232-240$$tJournal of aircraft$$v44$$x0021-8669
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000190318 9201_ $$0I:(DE-82)415110_20140620$$k415110$$lLehrstuhl für Strömungslehre und Aerodynamisches Institut$$x0
000190318 961__ $$c2014-08-12$$x2012-06-22$$z2012-02-20
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