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[null,"1.","Record Nr.",null,"UNINA9910796336203321"]
[null,null,"Autore",null,"Malherbe Philippe"]
[null,null,"Titolo",null,"Éléments de droit fiscal international / / Philippe Malherbe ; traduit de l'anglais par Olivier Malherbe"]
[null,null,"Pubbl/distr/stampa",null,"Bruxelles, [Belgium] : , : Bruylant, , 2015"]
[{"$nulls":4},"©2015"]
[null,null,"ISBN",null,"2-8027-5288-X"]
[null,null,"Descrizione fisica",null,"1 online resource (193 pages) : illustrations, tables"]
[null,null,"Disciplina",null,"343.052"]
[null,null,"Soggetti",null,"Income tax - Law and legislation"]
[{"$nulls":4},"Wages - Taxation - Law and legislation"]
[null,null,"Lingua di pubblicazione",null,"Francese"]
[null,null,"Formato",null,"Materiale a stampa"]
[null,null,null,"Livello bibliografico","Monografia"]
[null,null,null,"Nota di bibliografia","Includes bibliographical references."]
[null,"2.","Record Nr.",null,"UNINA9910815970503321"]
[null,null,"Autore",null,"Nazzeri Rahmetalla"]
[null,null,"Titolo",null,"Influence of flight control laws on structural sizing of commercial aircraft / / Rahmetalla Nazzeri"]
[null,null,"Pubbl/distr/stampa",null,"Göttingen : , : Cuvillier Verlag, , [2021]"]
[{"$nulls":4},"©2021"]
[null,null,"ISBN",null,"9783736965164"]
[{"$nulls":4},"9783736975163"]
[null,null,"Edizione",null,"[1st ed.]"]
[null,null,"Descrizione fisica",null,"1 online resource (181 pages)"]
[null,null,"Disciplina",null,"338.4762913334"]
[null,null,"Soggetti",null,"Aircraft industry"]
[null,null,"Lingua di pubblicazione",null,"Inglese"]
[null,null,"Formato",null,"Materiale a stampa"]
[null,null,null,"Livello bibliografico","Monografia"]
[null,null,null,"Nota di bibliografia","Includes bibliographical references."]
[null,null,"Nota di contenuto",null,"Intro -- 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 - "]
[{"$nulls":4},"basics -- F Influence of the load alleviationfunction on the calculated flightloads -- G Structural baseline generation -- H Influence of load alleviation functionon structural components."]