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Record Nr. |
UNINA9910465014803321 |
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Autore |
Nicolai Leland M (Leland Malcolm) |
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Titolo |
Fundamentals of aircraft and airship design . Volume 1 Aircraft design [[electronic resource] /] / Leland M. Nicolai, Grant E. Carichner |
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Pubbl/distr/stampa |
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Reston, Va., : American Institute of Aeronautics and Astronautics, 2010 |
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ISBN |
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1-60086-752-9 |
1-61344-046-4 |
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Descrizione fisica |
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1 online resource (931 p.) |
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Collana |
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Altri autori (Persone) |
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CarichnerGrant |
NicolaiLeland M (Leland Malcolm) |
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Disciplina |
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Soggetti |
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Airplanes - Design and construction - History |
Airships - Design and construction - History |
Aeronautics |
Electronic books. |
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Lingua di pubblicazione |
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Formato |
Materiale a stampa |
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Livello bibliografico |
Monografia |
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Note generali |
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Rev. and expanded ed. of: Fundamentals of aircraft design / Leland M. Nicolai. 1975. |
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Nota di bibliografia |
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Includes bibliographical references and index. |
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Nota di contenuto |
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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 |
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; |
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