Aircraft valuation in volatile market conditions : guiding toward profitability and prosperity / / Bijan Vasigh, Farshid Azadian |
Autore | Vasigh Bijan |
Pubbl/distr/stampa | Cham, Switzerland : , : Springer, , [2022] |
Descrizione fisica | 1 online resource (xxii, 468 pages) : illustrations |
Disciplina | 338.4762913334 |
Collana | Management for professionals |
Soggetto topico | Aircraft industry - Finance |
ISBN | 3-030-82450-0 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | Chapter 1. The Globalization and Evolution of the Aviation Industry Chapter 2. Aircraft Variants and Manufacturing Specifications Chapter 3. Aircraft Financial and Operational Efficiencies Chapter 4. The Foundation and Economics of Aircraft Valuation Chapter 5. A Step-By-Step Methodology for Commercial Aircraft Valuation: Case Study of Boeing and Airbus Chapter 6. The Principles of Long Term Financing and Effective Cost Management Chapter 7. Aircraft Secured Bond Transactions and SecuritizationChapter 8. General Aviation Aircraft Manufacturers and A ppraisalChapter 9. Aircraft Leasing and inanceChapter 10. Evaluation and Fleet Selection ProcessChapter 11. Aircraft Acquisition Trough Export Credit Agencies |
Record Nr. | UNINA-9910552743603321 |
Vasigh Bijan
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Cham, Switzerland : , : Springer, , [2022] | ||
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Lo trovi qui: Univ. Federico II | ||
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Airplane manufacturing in Farmingdale / / Ken Neubeck and Leroy E. Douglas ; with the Long Island Republic Airport Historical Society |
Autore | Neubeck Ken |
Pubbl/distr/stampa | Charleston, South Carolina : , : Arcadia Publishing, , 2016 |
Descrizione fisica | 1 online resource (232 pages) |
Disciplina | 338.4762913334 |
Collana | Images of aviation |
Soggetto topico |
Aircraft industry - New York (State) - Farmingdale - History
Aircraft industry - New York (State) - Farmingdale Aircraft industry |
Soggetto genere / forma | Electronic books. |
ISBN | 1-4396-5498-0 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910480548503321 |
Neubeck Ken
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Charleston, South Carolina : , : Arcadia Publishing, , 2016 | ||
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Lo trovi qui: Univ. Federico II | ||
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Airplane manufacturing in Farmingdale / / Ken Neubeck and Leroy E. Douglas ; with the Long Island Republic Airport Historical Society |
Autore | Neubeck Ken |
Pubbl/distr/stampa | Charleston, South Carolina : , : Arcadia Publishing, , 2016 |
Descrizione fisica | 1 online resource (232 pages) |
Disciplina | 338.4762913334 |
Collana | Images of aviation |
Soggetto topico |
Aircraft industry - New York (State) - Farmingdale - History
Aircraft industry - New York (State) - Farmingdale Aircraft industry |
ISBN | 1-4396-5498-0 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910798443103321 |
Neubeck Ken
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Charleston, South Carolina : , : Arcadia Publishing, , 2016 | ||
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Lo trovi qui: Univ. Federico II | ||
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Airplane manufacturing in Farmingdale / / Ken Neubeck and Leroy E. Douglas ; with the Long Island Republic Airport Historical Society |
Autore | Neubeck Ken |
Pubbl/distr/stampa | Charleston, South Carolina : , : Arcadia Publishing, , 2016 |
Descrizione fisica | 1 online resource (232 pages) |
Disciplina | 338.4762913334 |
Collana | Images of aviation |
Soggetto topico |
Aircraft industry - New York (State) - Farmingdale - History
Aircraft industry - New York (State) - Farmingdale Aircraft industry |
ISBN | 1-4396-5498-0 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910817171603321 |
Neubeck Ken
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Charleston, South Carolina : , : Arcadia Publishing, , 2016 | ||
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Lo trovi qui: Univ. Federico II | ||
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Influence of flight control laws on structural sizing of commercial aircraft / / Rahmetalla Nazzeri |
Autore | Nazzeri Rahmetalla |
Edizione | [1st ed.] |
Pubbl/distr/stampa | Göttingen : , : Cuvillier Verlag, , [2021] |
Descrizione fisica | 1 online resource (181 pages) |
Disciplina | 338.4762913334 |
Soggetto topico | Aircraft industry |
ISBN |
9783736965164
9783736975163 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | 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 - basics -- F Influence of the load alleviationfunction on the calculated flightloads -- G Structural baseline generation -- H Influence of load alleviation functionon structural components. |
Record Nr. | UNINA-9910795349903321 |
Nazzeri Rahmetalla
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Göttingen : , : Cuvillier Verlag, , [2021] | ||
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Lo trovi qui: Univ. Federico II | ||
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Influence of flight control laws on structural sizing of commercial aircraft / / Rahmetalla Nazzeri |
Autore | Nazzeri Rahmetalla |
Edizione | [1st ed.] |
Pubbl/distr/stampa | Göttingen : , : Cuvillier Verlag, , [2021] |
Descrizione fisica | 1 online resource (181 pages) |
Disciplina | 338.4762913334 |
Soggetto topico | Aircraft industry |
ISBN |
9783736965164
9783736975163 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | 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 - basics -- F Influence of the load alleviationfunction on the calculated flightloads -- G Structural baseline generation -- H Influence of load alleviation functionon structural components. |
Record Nr. | UNINA-9910815970503321 |
Nazzeri Rahmetalla
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Göttingen : , : Cuvillier Verlag, , [2021] | ||
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Lo trovi qui: Univ. Federico II | ||
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Sustainable aviation : a management perspective / / edited by Judith L. Walls, Andreas Wittmer |
Pubbl/distr/stampa | Cham, Switzerland : , : Springer, , [2022] |
Descrizione fisica | 1 online resource (222 pages) |
Disciplina | 338.4762913334 |
Collana | Management for Professionals |
Soggetto topico | Sustainable transportation |
ISBN | 3-030-90895-X |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910548172503321 |
Cham, Switzerland : , : Springer, , [2022] | ||
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Lo trovi qui: Univ. Federico II | ||
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