Aircraft : design, technology and safety / Collin Parker, editor.

Format:

Book

Contributor:

Parker, Collin, editor.

Series:

Transportation issues, policies and R&D series.

Transportation Issues, Policies and R&D

Standardized Title:

Aircraft (Nova Science Publishers)

Language:

English

Subjects (All):

Airplanes--Design and construction.

Airplanes.

Transport planes--Design and construction.

Transport planes.

Amphibian planes--Design and construction.

Amphibian planes.

Physical Description:

1 online resource (155 p.)

Place of Publication:

New York : Nova Publishers, 2015.

Language Note:

English

Summary:

In early stages of an aircraft design process, it is necessary to determine the minimum thrust or power requirement and rapidly select the appropriate propulsion, which involves a tight coupling between flight performance and missions' analyses, engine performance prediction and design optimization. The first chapter of this book provides an overview of how to determine the minimum thrust or power requirements for jet and propeller driver transport aircraft. The second chapter examines the comprehensive modeling and design of production processes of aircraft assembly. The final chapter focuses on the computational modeling of the Be-200 and Be-103 amphibious aircraft models.

Contents:

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

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

Chapter 2 COMPREHENSIVE MODELING AND DESIGN OF PRODUCTION PROCESSES OF AIRCRAFT ASSEMBLY ABSTRACT; 1. RUSSIAN SCIENTIFIC AND METHODOLOGICAL BASIS OF TECHNOLOGICAL DESIGN OF AN AIRFRAME ; 2. FEATURES OF DESIGN AND OPTIMIZATION OF AIRCRAFT ASSEMBLY IN MODERN CONDITIONS ; 3. THE COMPUTER AIDED SYSTEM OF DESIGN OF TECHNOLOGICAL PROCESSES "ТЕМП" ; 4. MODELS OF DESIGN AND OPTIMIZATION OF ASSEMBLY ; Mathematical Economic Models ; Electronic Models of Objects and Processes of Assembly ; Models of Management of Product Configurations ; Simulation Models of Assembly Production

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

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

Notes:

Description based upon print version of record.

Includes bibliographical references at the end of each chapters and index.

Description based on print version record.

ISBN:

1-63483-357-0