Aircraft design
Saved in:
Main Author: | |
---|---|
Format: | eBook |
Language: | English |
Published: |
Cambridge ; New York :
Cambridge University Press,
2010.
|
Series: | Cambridge aerospace series.
|
Subjects: | |
ISBN: | 9780511677854 9780511685569 9780511844652 |
Physical Description: | 1 online zdroj (xlii, 606 p.) : ill. |
LEADER | 04921cam a2200385 a 4500 | ||
---|---|---|---|
001 | 73842 | ||
003 | CZ ZlUTB | ||
005 | 20240911211744.0 | ||
006 | m d | ||
007 | cr un | ||
008 | 090723s2010 enka sb 001 0 eng d | ||
020 | |a 9780511677854 |q (ebook) | ||
020 | |a 9780511685569 |q (ebook) | ||
020 | |a 9780511844652 |q (ebook) | ||
035 | |a (OCoLC)647925909 |z (OCoLC)642206059 |z (OCoLC)741249733 |z (OCoLC)746752556 |z (OCoLC)818664645 | ||
040 | |a E7B |b eng |c E7B |d CDX |d CEF |d OCLCQ |d N$T |d YDXCP |d OCLCQ |d IDEBK |d KNOVL |d ZCU |d DEBSZ |d OCLCQ |d B24X7 |d OCLCQ |d CAMBR |d KNOVL | ||
100 | 1 | |a Kundu, Ajoy Kumar, |d 1932- | |
245 | 1 | 0 | |a Aircraft design |h [elektronický zdroj] / |c Ajoy Kumar Kundu. |
260 | |a Cambridge ; |a New York : |b Cambridge University Press, |c 2010. | ||
300 | |a 1 online zdroj (xlii, 606 p.) : |b ill. | ||
490 | 1 | |a Cambridge aerospace series | |
504 | |a Includes bibliographical references and index. | ||
505 | 0 | |a Cover -- Half-title -- Series-title -- Title -- Copyright -- Contents -- Symbols and Abbreviations -- Symbols -- Greek Symbols -- Subscripts -- Abbreviations -- Preface -- Road Map of the Book -- The Arrangement -- Suggested Route for the Coursework -- First Semester -- Second Semester -- Suggestions for the Class -- Use of Semi-empirical Relations -- 1 Introduction -- 1.1 Overview -- 1.1.1 What Is to Be Learned? -- 1.1.2 Coursework Content -- 1.2 Brief Historical Background -- 1.3 Current Aircraft Design Status -- 1.3.1 Forces and Drivers -- 1.3.2 Current Civil Aircraft Design Trends -- 1.3.3 Current Military Aircraft Design Trends -- 1.4 Future Trends -- 1.4.1 Civil Aircraft Design: Future Trends -- 1.4.2 Military Aircraft Design: Future Trends -- 1.5 Learning Process -- 1.6 Units and Dimensions -- 1.7 Cost Implications -- 2 Methodology to Aircraft Design, Market Survey, and Airworthiness -- 2.1 Overview -- 2.1.1 What Is to Be Learned? -- 2.1.2 Coursework Content ---2.2 Introduction -- 2.3 Typical Design Process -- 2.3.1 Four Phases of Aircraft Design -- 2.3.2 Typical Resources Deployment -- 2.3.3 Typical Cost Frame -- 2.3.4 Typical Time Frame -- 2.4 Typical Task Breakdown in Each Phase -- Phase 1: Conceptual Study Phase (Feasibility Study) -- Phase 2: Project Definition Phase (Preliminary Design) -- Phase 3: Detailed Design Phase (Full-Scale Product Development) -- Phase 4: Final Phase (Certification) -- 2.4.1 Functional Tasks during the Conceptual Study (Phase 1: Civil Aircraft) -- 2.4.2 Project Activities for Small Aircraft Design -- 2.5 Aircraft Familiarization -- 2.5.1 Civil Aircraft and Its Component Configurations -- 2.5.2 Military Aircraft and Its Component Configurations -- 2.6 Market Survey -- 2.7 Civil Aircraft Market -- 2.7.1 Aircraft Specifications and Requirements for Three Civil Aircraft Case Studies -- 2.8 Military Market -- 2.8.1 Aircraft Specifications/Requirements for Military Aircraft Case Studies ---2.9 Comparison between Civil and Military Aircraft Design Requirements -- 2.10 Airworthiness Requirements -- 2.11 Coursework Procedures -- 3 Aerodynamic Considerations -- 3.1 Overview -- 3.1.1 What Is to Be Learned? -- 3.1.2 Coursework Content -- 3.2 Introduction -- 3.3 Atmosphere -- 3.4 Fundamental Equations -- 3.5 Airflow Behavior: Laminar and Turbulent -- 3.5.1 Flow Past Aerofoil -- 3.6 Aircraft Motion and Forces -- 3.6.1 Motion -- 3.6.2 Forces -- 3.7 Aerofoil -- 3.7.1 Groupings of Aerofoils and Their Properties -- 3.8 Definitions of Aerodynamic Parameters -- 3.9 Generation of Lift -- 3.10 Types of Stall -- 3.10.1 Gradual Stall -- 3.10.2 Abrupt Stall -- 3.11 Comparison of Three NACA Aerofoils -- 3.12 High-Lift Devices -- 3.13 Transonic Effects Area Rule -- 3.14 Wing Aerodynamics -- 3.14.1 Induced Drag and Total Aircraft Drag -- 3.15 Aspect Ratio Correction of 2D Aerofoil Characteristics for 3D Finite Wing -- 3.16 Wing Definitions -- 3.16.1 Planform Area, SW ---3.16.2 Wing Aspect Ratio -- 3.16.3 Wing Sweep Angle, A -- 3.16.4 Wing Root (Croot) and Tip (Ctip) Chord -- 3.16.5 Wing Taper Ratio, Lambda -- 3.16.6 Wing Twist -- 3.16.7 HighLow Wing -- 3.16.8 DihedralAnhedral Angles -- 3.17 Mean Aerodynamic Chord -- 3.18 Compressibilit. | |
588 | |a Description based on print version record. | ||
506 | |a Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty univerzity | ||
650 | 0 | |a Airplanes |x Design and construction. | |
650 | 0 | |a Aeronautics. | |
655 | 7 | |a elektronické knihy |7 fd186907 |2 czenas | |
655 | 9 | |a electronic books |2 eczenas | |
776 | 0 | 8 | |i Print version: |a Kundu, Ajoy Kumar, 1932- |t Aircraft design. |d Cambridge ; New York : Cambridge University Press, 2010 |w (DLC) 2009027795 |
830 | 0 | |a Cambridge aerospace series. | |
856 | 4 | 0 | |u https://proxy.k.utb.cz/login?url=http://app.knovel.com/web/toc.v/cid:kpAD000013 |y Plný text |
992 | |a BK |c KNOVEL | ||
999 | |c 73842 |d 73842 | ||
993 | |x NEPOSILAT |y EIZ |