LEADER 01747nas 2200541- 450 001 996335987103316 005 20231213213019.0 035 $a(CKB)991042727086158 035 $a(CONSER)--2001215162 035 $a(EXLCZ)99991042727086158 100 $a20010709a20019999 --- a 101 0 $aeng 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 00$aHealthLeaders 210 1$cHealthLeaders, Inc.,$d2001- 210 31$aBrentwood, TN :$cHealthLeaders Media 215 $a1 online resource 300 $a"Information to lead", <2002-> 300 $aIssues for <2005-> published in Nashville, TN. 311 08$aPrint version: HealthLeaders. 1536-1357 (DLC) 2001215162 (OCoLC)47260920 517 3 $aHealth leaders 531 0 $aHealthLeaders 606 $aMedical economics$vPeriodicals 606 $aMedical care$vPeriodicals 606 $aMedical care$xFinance$vPeriodicals 606 $aHealth Facility Administration 606 $aHealth Facilities$xeconomics 606 $aMedical care$2fast$3(OCoLC)fst01013753 606 $aMedical care$xFinance$2fast$3(OCoLC)fst01013800 606 $aMedical economics$2fast$3(OCoLC)fst01014004 608 $aPeriodical. 608 $aPeriodicals.$2fast 615 0$aMedical economics 615 0$aMedical care 615 0$aMedical care$xFinance 615 12$aHealth Facility Administration. 615 22$aHealth Facilities$xeconomics. 615 7$aMedical care. 615 7$aMedical care$xFinance. 615 7$aMedical economics. 712 02$aHealthLeaders, Inc., 906 $aJOURNAL 912 $a996335987103316 920 $aexl_impl conversion 996 $aHealthLeaders$92021138 997 $aUNISA LEADER 03275nam 2200421 450 001 9910815970503321 005 20230630001411.0 010 $a9783736965164$b(electronic bk.) 010 $z9783736975163 035 $a(MiAaPQ)EBC6805965 035 $a(Au-PeEL)EBL6805965 035 $a(OCoLC)1285783061 035 $a(CKB)19434192500041 035 $a(EXLCZ)9919434192500041 100 $a20220811d2021 uy 0 101 0 $aeng 135 $aurcnu|||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aInfluence of flight control laws on structural sizing of commercial aircraft /$fRahmetalla Nazzeri 205 $a1st ed. 210 1$aGo?ttingen :$cCuvillier Verlag,$d[2021] 210 4$d©2021 215 $a1 online resource (181 pages) 311 08$aPrint version: Nazzeri, Rahmetalla Influence of flight control laws on structural sizing of commercial aircraft Göttingen : Cuvillier Verlag,c2021 9783736975163 320 $aIncludes bibliographical references. 327 $aIntro -- List of Figures -- List of Tables -- List of symbols -- 1 Introduction -- 1.1 The need for a new simulation framework -- 1.2 State of the art -- 1.3 Objectives and thesis overview -- 2 Multidisciplinary analysis andoptimization framework -- 2.1 Developed process and mixture of competences -- 2.2 General process overview -- 3 Loads calculation process -- 3.1 Scope of computed load conditions -- 3.2 Loads calculation model -- 3.3 Electronic Flight Control System -- 4 Structural property optimization andmass penalty estimation -- 4.1 Modeling aspects of global FEM representation -- 4.2 Global FEM external loading -- 4.3 Linear static analysis and results management -- 4.4 Wing structural property optimization -- 4.5 Fuselage mass penalty estimation -- 5 Feedback loop -- 5.1 Starting approach -- 5.2 Main process steps of the feedback loop -- 5.3 Update of stiffness values - equivalent beamapproach -- 5.4 Update of mass values - grid point weight generator -- 5.5 Global convergence criteria -- 5.6 Impact of wing stiffness changes on the jig and flightshape -- 6 Design studies -- 6.1 Influence of the load alleviation function on thecalculated flight loads -- 6.2 First design study with reduced load case set -- 6.3 Design study with complete load case set -- 7 Summary, discussion of methods andresults, outlook -- 7.1 Summary -- 7.2 Discussion of methods -- 7.3 Discussion of results -- 7.4 Outlook -- Bibliography -- A Loads calculation and structuralassessment -- B Feedback loop - main process steps -- C Equivalent beam approach -validation -- D Equivalent beam approach -influence of skin and stringer -- E Grid Point Weight Generator - basics -- F Influence of the load alleviationfunction on the calculated flightloads -- G Structural baseline generation -- H Influence of load alleviation functionon structural components. 606 $aAircraft industry 615 0$aAircraft industry. 676 $a338.4762913334 700 $aNazzeri$b Rahmetalla$01644330 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 912 $a9910815970503321 996 $aInfluence of flight control laws on structural sizing of commercial aircraft$93990139 997 $aUNINA LEADER 01272nam0 22002651i 450 001 UON00381339 005 20231205104529.150 010 $a95-19-50742-6 100 $a20100511d1977 |0itac50 ba 101 $aeng$aHEB 102 $aFI 105 $a|||| ||||| 200 1 $aOn the vocalism of the closed unstressed syllables in Hebrew$ea study based on the evidence provided by the transcriptions of St. Jerome and Palestinian punctuations$fby Tapani Harviainen 210 $aHelsinki$cSocietas Orientalis Fennica$d1977 215 $axvii, 263, 6, 6 p.$d25 cm. 461 1$1001UON00101067$12001 $aStudia Orientalia$fSocietas Orientalis Fennica$1205 $aVol. 1 (1925)- $1207 $aHelsinki : Helsingforsiae : [poi] Societas Orientalis Fennica, 1925- $1210 $av.$a26 cm$1215 $aPeriodicitŕ irregolare$vv.48,1977 606 $aLingua ebraica$xMorfologia e sintassi$3UONC015296$2FI 620 $aFI$dHelsinki$3UONL000062 686 $aSEB II C$cSTUDI EBRAICI - 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