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Aircraft : design, technology and safety /

Detalles Bibliográficos
Clasificación:Libro Electrónico
Otros Autores: Parker, Collin (Editor )
Formato: Electrónico eBook
Idioma:Inglés
Publicado: New York : Nova Publishers, [2015]
Colección:Transportation issues, policies and R & D series.
Temas:
Acceso en línea:Texto completo

MARC

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130 0 |a Aircraft (Nova Science Publishers) 
245 1 0 |a Aircraft :  |b design, technology and safety /  |c Collin Parker, editor. 
264 1 |a New York :  |b Nova Publishers,  |c [2015] 
300 |a 1 online resource 
336 |a text  |b txt  |2 rdacontent 
337 |a computer  |b c  |2 rdamedia 
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490 1 |a Transportation issues, policies and R & D 
504 |a Includes bibliographical references (pages 131-138) and index. 
588 0 |a Print version record. 
505 0 |a AIRCRAFT DESIGN, TECHNOLOGY AND SAFETY ; AIRCRAFT DESIGN, TECHNOLOGY AND SAFETY ; Library of Congress Cataloging-in-Publication Data; CONTENTS ; PREFACE ; Chapter 1 POWER REQUIREMENTS v ; ABSTRACT; 1. INTRODUCTION ; 2. AIRCRAFT CONCEPTUAL DESIGN ; 3. PROPULSION REQUIREMENTS ; 4. AIRCRAFT CONFIGURATION AND AERODYNAMICS ; 5. FLIGHT MISSIONS CONSTRAINTS ANALYSES ; 5.1. Flight Missions' Envelope ; 5.2. Takeoff Performance ; 5.3. Climb in Takeoff Performance ; 5.4. Climb in Altitude Performance ; 5.5. Climb Performance for a Propeller-Driven Aircraft ; 5.6. Cruising Performance 
505 8 |a 5.7. Performance of Landing 5.8. Diagram of Constraints ; 5.9. Optimum Match-Point ; 6. AIRCRAFT ENGINE MODELING, SIMULATION AND DESIGN OPTIMIZATION ; 7. ENGINES GAS POWER MODELING AND OPTIMIZATION ; 7.1. On-Design Performance ; 7.2. Off-Design Performance ; 7.3. Design Optimization ; 7.4. Turbofan Optimization Results ; 7.5. Turboprop Optimization Results ; Single Shaft Fixed Turbine Turboprop ; Single Shaft Free Turbine Turboprop ; Twin Shaft Fixed Turbine Turboprop ; CONCLUSION ; NOMENCLATURE ; Subscripts ; Greek Script ; ABBREVIATIONS ; REFERENCES 
505 8 |a Models of Calculation of Manufacturability Parameters 5. DEVELOPMENT OF ASSEMBLY TECHNOLOGY OF A WING OF AN AIRCRAFT USING IAS TPP ; The Simulation Model of the Production Process of the Wingbox Assembly; REFERENCES ; Chapter 3 COMPUTATIONAL MODELING OF AMPHIBIOUS AIRCRAFT BE-200 AND BE-103 ; ABSTRACT ; INTRODUCTION ; 1. HISTORICAL STAGES OF HYDROAVIATION DEVELOPMENT BY THE BERIEV AIRCRAFT COMPANY ; 2. COMPUTATIONAL MODELING OF AMPHIBIOUS AIRCRAFT BE-200 ; 2.1. Introduction ; 2.2. Modeling Methods and Stages ; 2.3. Shading and Rendering of 3D Model 
505 8 |a 3. COMPUTATIONAL MODELING OF AMPHIBIOUS AIRCRAFT BE-103 3.1. Introduction ; 3.2. Modeling methods and Stages ; 3.3. Shading and Rendering of 3D-Model ; CONCLUSION ; REFERENCES ; BIBLIOGRAPHY ; INDEX 
590 |a eBooks on EBSCOhost  |b EBSCO eBook Subscription Academic Collection - Worldwide 
650 0 |a Airplanes  |x Design and construction. 
650 0 |a Transport planes  |x Design and construction. 
650 0 |a Amphibian planes  |x Design and construction. 
650 6 |a Avions  |x Conception et construction. 
650 7 |a TECHNOLOGY & ENGINEERING  |x Engineering (General)  |2 bisacsh 
650 7 |a Transport planes  |x Design and construction  |2 fast 
650 7 |a Airplanes  |x Design and construction  |2 fast 
700 1 |a Parker, Collin,  |e editor. 
776 0 8 |i Print version:  |t Aircraft.  |d New York : Nova Publishers, [2015]  |z 9781634833363  |w (DLC) 2015024650 
830 0 |a Transportation issues, policies and R & D series. 
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