Autorentext
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/

Klappentext

Features: 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

Inhalt

1. Aircraft design process

   2. Aircraft cost analysis
   3. Initial sizing
   4. Aircraft conceptual layout
   5. Aircraft structural layout
   6. Aircraft weight analysis
   7. Selecting the power plant
   8. The anatomy of the airfoil
   9. The anatomy of the wing
   10. The anatomy of lift enhancement
   11. The anatomy of the tail
   12. The anatomy of the fuselage
   13. The anatomy of the landing gear
   14. Thrust modeling for gas turbines
   15. Thrust modeling for propellers
   16. Aircraft drag analysis
   17. Performance - introduction
   18. Performance - take-off
   19. Performance - climb
   20. Performance - cruise
   21. Performance - range analysis
   22. Performance - descent
   23. Performance - landing
   24. Longitudinal stability and control
   25. Lat-dir stability and control
   26. Miscellaneous design notes

   Appendix
   A. Atmospheric modeling
   B. Aerospace engineer's formula sheet
   C. Design of biplanes and seaplanes
   D. Derivation of landing side-constraint