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E-raamat: General Aviation Aircraft Design: Applied Methods and Procedures

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(Department of Aerospace Engineering, Embry-Riddle Aeronautical University, FL, USA)
  • Formaat: PDF+DRM
  • Ilmumisaeg: 31-Oct-2021
  • Kirjastus: Butterworth-Heinemann Inc
  • Keel: eng
  • ISBN-13: 9780128226476
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General Aviation Aircraft Design: Applied Methods and ProceduresSuurem pilt
  • Formaat: PDF+DRM
  • Ilmumisaeg: 31-Oct-2021
  • Kirjastus: Butterworth-Heinemann Inc
  • Keel: eng
  • ISBN-13: 9780128226476
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General Aviation Aircraft Design, Second Edition, continues to be the engineer’s best source for answers to realistic aircraft design questions. The book has been expanded to provide design guidance for additional classes of aircraft, including seaplanes, biplanes, UAS, high-speed business jets, and electric airplanes. In addition to conventional powerplants, design guidance for battery systems, electric motors, and complete electric powertrains is offered. The second edition contains new chapters:

  • Thrust Modeling for Gas Turbines
  • Longitudinal Stability and Control
  • Lateral and Directional Stability and Control

These new chapters offer multiple practical methods to simplify the estimation of stability derivatives and introduce hinge moments and basic control system design. Furthermore, all chapters have been reorganized and feature updated material with additional analysis methods. This edition also provides an introduction to design optimization using a wing optimization as an example for the beginner.

Written by an engineer with more than 25 years of design experience, professional engineers, aircraft designers, aerodynamicists, structural analysts, performance analysts, researchers, and aerospace engineering students will value the book as the classic go-to for aircraft design.

  • The printed book is now in color, with 1011 figures and illustrations!
  • Presents the most common methods for conceptual aircraft design
  • Clear presentation splits text into shaded regions, separating engineering topics from mathematical derivations and examples
  • Design topics range from the "new" 14 CFR Part 23 to analysis of ducted fans. All chapters feature updated material with additional analysis methods. Many chapters have been reorganized for further help. Introduction to design optimization is provided using a wing optimization as an example for the beginner
  • Three new chapters are offered, two of which focus on stability and control. These offer multiple practical methods to simplify the estimation of stability derivatives. The chapters introduce hinge moments and basic control system design
  • Real-world examples using aircraft such as the Cirrus SR-22 and Learjet 45

Arvustused

"Gudmundsson has set a benchmark for textbooks on aircraft design. Within its declared bounds this book is remarkably comprehensive, with introductory material, clearly presented mathematical tools with assumptions and derivations, notes on when and where to apply them and numerous real-world examples.

Gudmundsson truly has a feel for design, something he tries to convey throughout, describing each task, the nature of the designers approach and the wide-ranging set of constraints to be addressed. As well as all the analytical work described above, aircraft design requires graphic skills. A real pleasure in this book is the high quality of the illustrations; Gudmundsson is right to be proud of them.

Of the many textbooks on aircraft design this is my favourite. The authors declared aim remained, as with the first edition, to gather information and procedures helpful to the designer. He has achieved this to a very impressive standard. By including all aspects, even organisation and management of the process, he has made this a valuable and comprehensive go-to reference source." --John M Robertson, CEng MIMechE MRAeS, RAeS General Aviation Group

Preface to the 1st Edition   xi  
Preface to the 2nd Edition   xiii  
Acknowledgments for the 1st Edition   xv  
Acknowledgments for the 2nd Edition   xvii  
Helpful Notes   xix  
  1 The Aircraft Design Process
 
  1.1 Introduction
  1 (1)
  1.2 General Process of Aircraft Design and Development
  2 (8)
  1.3 Introduction to Aviation Regulations and Certification
  10 (5)
  1.4 How to Design a New Aircraft
  15 (3)
  1.5 Elements of Project Engineering
  18 (9)
  1.6 Presenting the Design Project
  27 (6)
  References
  32 (1)
  2 Aircraft Cost Analysis
 
  2.1 Introduction
  33 (5)
  2.2 The Estimation of Project Development Costs
  38 (12)
  2.3 Estimating Aircraft Operational Costs
  50 (7)
  Exercises
  55 (1)
  References
  55 (2)
  3 Initial Sizing
 
  3.1 Introduction
  57 (1)
  3.2 Constraint Analysis
  58 (11)
  3.3 Introduction to Trade Studies
  69 (4)
  3.4 Introduction to Design Optimization
  73 (20)
  Exercises
  89 (2)
  References
  91 (2)
  4 Aircraft Configuration Layout
 
  4.1 Introduction
  93 (7)
  4.2 The Fundamentals of the Configuration Layout
  100 (13)
  References
  111 (2)
  5 Aircraft Structural Layout
 
  5.1 Introduction
  113 (1)
  5.2 Aircraft Fabrication and Materials
  114 (16)
  5.3 Airframe Structural Layout
  130 (17)
  References
  145 (2)
  6 Aircraft Weight Analysis
 
  6.1 Introduction
  147 (2)
  6.2 Initial Weight Analysis Methods
  149 (10)
  6.3 Secondary Weight Analysis Methods
  159 (1)
  6.4 Statistical Weight Estimation Methods
  160 (7)
  6.5 Direct Weight Estimation Methods
  167 (9)
  6.6 Inertia Properties
  176 (7)
  6.7 The Center-of-Gravity Envelope
  183 (14)
  Exercises
  194 (1)
  References
  195 (2)
  7 Selecting the Powerplant
 
  7.1 Introduction
  197 (5)
  7.2 Piston Engines
  202 (23)
  7.3 Gas Turbine Engines
  225 (14)
  7.4 Electric Motors and Battery Technology
  239 (18)
  Exercises
  253 (1)
  References
  253 (4)
  8 The Anatomy of the Airfoil
 
  8.1 Introduction
  257 (25)
  8.2 The Geometry of the Airfoil
  282 (17)
  8.3 The Force and Moment Characteristics of the Airfoil
  299 (23)
  Exercises
  317 (1)
  References
  317 (5)
  9 The Anatomy of the Wing
 
  9.1 Introduction
  322 (1)
  9.2 The Trapezoidal Wing Planform
  322 (8)
  9.3 The Geometric Layout of the Wing
  330 (20)
  9.4 Planform Selection
  350 (13)
  9.5 Lift and Moment Characteristics of Wings
  363 (25)
  9.6 Wing Stall Characteristics
  388 (11)
  9.7 Prandtl's Lifting-Line Theory
  399 (16)
  Exercises
  412 (1)
  References
  412 (3)
  10 The Anatomy of Lift Enhancement
 
  10.1 Introduction
  415 (1)
  10.2 Leading-Edge High-Lift Devices
  416 (16)
  10.3 Trailing-Edge High-Lift Devices
  432 (24)
  10.4 Effect of Deploying High-Lift Devices on Wings
  456 (5)
  10.5 Wingtip Design
  461 (20)
  References
  477 (4)
  11 The Anatomy of the Tail
 
  11.1 Introduction
  481 (2)
  11.2 The Geometry of the Tail
  483 (8)
  11.3 On the Pros and Cons of Tail Configurations
  491 (14)
  11.4 Initial Tail Sizing Methods
  505 (12)
  Exercises
  516 (1)
  References
  516 (1)
  12 The Anatomy of the Fuselage
 
  12.1 Introduction
  517 (2)
  12.2 Fundamentals of Fuselage Shapes
  519 (2)
  12.3 Sizing the Fuselage
  521 (8)
  12.4 Estimating the Geometric Properties of the Fuselage
  529 (6)
  12.5 Additional Information
  535 (6)
  References
  539 (2)
  13 The Anatomy of the Landing Gear
 
  13.1 Introduction
  541 (3)
  13.2 Tires, Wheels, and Brakes
  544 (15)
  13.3 Geometric Layout of the Landing Gear
  559 (14)
  References
  571 (2)
  14 Thrust Modeling for Gas Turbines
 
  14.1 Introduction
  573 (8)
  14.2 Theory of Reactive Thrust
  581 (7)
  14.3 General Thrust Modeling for Gas Turbines
  588 (9)
  Exercises
  595 (1)
  References
  595 (2)
  15 Thrust Modeling for Propellers
 
  15.1 Introduction
  597 (11)
  15.2 Propeller Effects
  608 (12)
  15.3 Properties and Selection of the Propeller
  620 (10)
  15.4 Determination of Propeller Thrust
  630 (8)
  15.5 Rankine-Froude Momentum Theory
  638 (8)
  15.6 Blade Element Theory
  646 (12)
  References
  656 (2)
  16 Aircraft Drag Analysis
 
  16.1 Introduction
  658 (1)
  16.2 The Basics of Drag Modeling
  659 (19)
  16.3 Estimating the Drag of a Complete Aircraft
  678 (34)
  16.4 Miscellaneous or Additive Drag
  712 (24)
  16.5 Special Topics Involving Drag
  736 (8)
  16.6 Additional Information--Drag of Selected Aircraft
  744 (9)
  Exercises
  745 (5)
  References
  750 (3)
  17 Performance--Introduction
 
  17.1 Introduction
  753 (3)
  17.2 Atmospheric Modeling
  756 (4)
  17.3 Airspeed Theory
  760 (9)
  17.4 The Structural Envelope
  769 (9)
  17.5 Sample Aircraft
  778 (7)
  Exercises
  783 (1)
  References
  784 (1)
  18 Performance--Take-Off
 
  18.1 Introduction
  785 (5)
  18.2 Fundamental Relations for the Take-Off Run
  790 (5)
  18.3 Conducting the Take-Off Analysis
  795 (13)
  18.4 Database--T-O Perfonnance of Selected Aircraft
  808 (3)
  Exercises
  809 (1)
  References
  810 (1)
  19 Performance--Climb
 
  19.1 Introduction
  811 (1)
  19.2 Fundamental Relations for the Climb Maneuver
  812 (3)
  19.3 General Climb Analysis Methods
  815 (15)
  19.4 Aircraft Database--Rate-of-Climb of Selected Aircraft
  830 (3)
  References
  832 (1)
  20 Performance--Cruise
 
  20.1 Introduction
  833 (1)
  20.2 Fundamental Relations for the Cruise Maneuver
  834 (5)
  20.3 General Cruise Analysis Methods for Steady Flight
  839 (20)
  20.4 General Analysis Methods for Accelerated Flight
  859 (8)
  References
  866 (1)
  21 Performance--Range and Endurance
 
  21.1 Introduction
  867 (1)
  21.2 Fundamental Relations for Range and Endurance
  868 (5)
  21.3 Range Analysis
  873 (11)
  21.4 Endurance Analysis
  884 (2)
  21.5 Analysis of Mission Profile
  886 (7)
  Exercises
  890 (1)
  References
  890 (3)
  22 Performance--Descent
 
  22.1 Introduction
  893 (1)
  22.2 Fundamental Relations for the Descent Maneuver
  894 (1)
  22.3 General Descent Analysis Methods
  895 (5)
  22.4 Sailplane Glide Performance
  900 (15)
  References
  914 (1)
  23 Performance--Landing
 
  23.1 Introduction
  915 (2)
  23.2 Fundamental Relations for the Landing Phase
  917 (6)
  23.3 Database--Landing Performance of Selected Aircraft
  923 (2)
  References
  924 (1)
  24 Longitudinal Stability and Control
 
  24.1 Introduction
  925 (6)
  24.2 Static Longitudinal Stability and Control
  931 (26)
  24.3 Refined Horizontal Tail Sizing
  957 (9)
  24.4 Introduction to Hinge Moments
  966 (9)
  References
  973 (2)
  25 LAT-DIR Stability and Control
 
  25.1 Introduction
  975 (1)
  25.2 Lateral-Directional Stability and Control
  975 (4)
  25.3 Directional Stability and Control
  979 (9)
  25.4 Lateral Stability and Control
  988 (11)
  25.5 Basics of Roll and Yaw Control
  999 (8)
  References
  1005 (2)
  26 Miscellaneous Design Notes
 
  26.1 Introduction
  1007 (1)
  26.2 General Aviation Aircraft Design Checklist
  1007 (10)
  26.3 Faults and Fixes
  1017 (14)
  References
  1029 (2)
Appendix A Atmospheric Modeling   1031 (8)
Appendix B The Aerospace Engineer's Formula Sheet   1039 (10)
Appendix C Design of Biplanes and Seaplanes   1049 (26)
Appendix D Derivation of Landing Side-Constraint   1075 (4)
Index   1079  
Dr. Snorri Gudmundsson served from 1995-2009 at Cirrus Aircraft. He served in various engineering roles in the development of several aircraft, including the Cirrus SR20 and SR22 aircraft. From 2005-2009, he served as the Chief Aerodynamicist, where he was responsible for the aerodynamics of the SF50 Vision jet (recipient of the 2017 Collier Trophy). He had two appointments a Designated Engineering Representative (DER) for the FAA, as a Structural and Flight Analyst. He has contributed to the certification of several aircraft. This includes development and certification flight and structural testing. He has conducted load analysis, stability and control evaluation, and performance analysis on a variety of single and multi-engine aircraft. In 2010, Dr. Gudmundsson joined the faculty at Embry-Riddle Aeronautical University, where he is currently an Associate Professor of Aerospace Engineering, teaching aircraft design and aerodynamics. Dr. Snorri has a Youtube channel on Aircraft Design: https://www.youtube.com/channel/UCS0O5jdhFrdYBFC5YJP6axg/
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