{"text_format":"2","workbook":"xls","n_sheets":1,"sheets":["report2"],"not_rendered":{"charts":0,"images":0,"macros":0,"external_links":1,"defined_names":1,"comments":0,"pivot_tables":0},"unopened":[],"bounds":{"document_bytes":16777216,"sheet_cells":100000,"run_cost":"one","rows_first":2000,"rows_last":500,"rows_between":2000,"halvings":0,"cell_chars":16384,"cell_head_chars":4096},"cells_cut":0,"cells_raw":0,"read":"whole","date_system":"1900","formulas":"cached_only"}

{"sheet":"report2","index":0,"n_rows":23,"n_cols":5,"rows_kept":23,"cut":false,"hidden":false,"merged":[[0,2,0,3],[0,4,0,5],[1,2,1,3],[1,4,1,5],[2,2,2,3],[2,4,2,5],[3,2,3,3],[4,2,4,3],[6,2,6,3],[7,2,7,3],[8,2,8,3],[9,2,9,3],[10,2,10,3],[13,2,13,3],[14,2,14,3],[18,2,18,3]],"flags":["formulas_cached_only"]}
[null,"1.","Record Nr.",null,"UNINA9910967130603321"]
[null,null,"Autore",null,"Nicolai Leland M (Leland Malcolm)"]
[null,null,"Titolo",null,"Fundamentals of aircraft and airship design . Volume 1 Aircraft design / / Leland M. Nicolai, Grant E. Carichner"]
[null,null,"Pubbl/distr/stampa",null,"Reston, Va., : American Institute of Aeronautics and Astronautics, 2010"]
[null,null,"ISBN",null,"1-60086-752-9"]
[{"$nulls":4},"1-61344-046-4"]
[null,null,"Edizione",null,"[1st ed.]"]
[null,null,"Descrizione fisica",null,"1 online resource (931 p.)"]
[null,null,"Collana",null,"AIAA educational series"]
[null,null,"Disciplina",null,"629.134/1"]
[null,null,"Soggetti",null,"Airplanes - Design and construction - History"]
[{"$nulls":4},"Airships - Design and construction - History"]
[{"$nulls":4},"Aeronautics"]
[null,null,"Lingua di pubblicazione",null,"Inglese"]
[null,null,"Formato",null,"Materiale a stampa"]
[null,null,null,"Livello bibliografico","Monografia"]
[null,null,null,"Note generali","Rev. and expanded ed. of: Fundamentals of aircraft design / Leland M. Nicolai. 1975."]
[null,null,null,"Nota di bibliografia","Includes bibliographical references and index."]
[null,null,"Nota di contenuto",null,"COVER; TITLE; COPYRIGHT; FOREWORD; CONTENTS; LIST OF COLOR PLATES; PREFACE; Chapter 1: Introduction; Chapter 2: Review of Practical Aerodynamics; Chapter 3: Aircraft Performance Methods; Chapter 4: Aircraft Operating Envelope; Chapter 5: Preliminary Estimate of Takeoff Weight; Chapter 6: Estimating theTakeoff Wing Loading; Chapter 7: Selecting the Planform and Airfoil Section; Chapter 8: Preliminary Fuselage Sizing and Design; Chapter 9: High-Lift Devices; Chapter 10: Takeoff and Landing Analysis; Chapter 11: Preliminary Sizing of the Vertical and Horizontal Tails"]
[{"$nulls":4},"Chapter 12: Designing for Survivability (Stealth)Chapter 13: Estimating Wing-Body Aerodynamics; Chapter 14: Propulsion System Fundamentals; Chapter 15: Turbine Engine Inlet Design; Chapter 16: Corrections forTurbine Engine Installation; Chapter 17: Propeller Propulsion Systems; Chapter 18: Propulsion System Thrust Sizing; Chapter 19: Structures and Materials; Chapter 20: Refined Weight Estimate; Chapter 21 Static Stability and Control; Chapter 22: Trim Drag and Maneuvering Flight; Chapter 23: Control Surface Sizing Criteria; Chapter 24: Life Cycle Cost; Chapter 25: Trade Studies and Sizing"]
[{"$nulls":4},"Appendix A: ConversionsAppendix B: Atmospheric Data; Appendix C: Isentropic Compressible Flow Functions; Appendix D: Normal Shock Functions for a Perfect Gas; Appendix E: Plane Oblique and Conical Shocks; Appendix F: NACA Airfoil Nomenclature and Data; Appendix G: Aerodynamic Data of Real Aircraft; Appendix H: Aerodynamics of Wing-"]
[{"$nulls":4},"Body Combinations; Appendix I: Aircraft Weights Data; Appendix J: Propulsion Data; Appendix K: Miscellaneous Data; INDEX; SUPPORTING MATERIALS"]
[null,null,null,"Sommario/riassunto","The aircraft is only a transport mechanism for the payload, and all design decisions must consider payload first. Simply stated, the aircraft is a dust cover. \"Fundamentals of Aircraft and Airship Design, Volume 1: Aircraft Design\" emphasizes that the science and art of the aircraft design process is a compromise and that there is no right answer; however, there is always a best answer based on existing requirements and available technologies."]