Fundamentals of aircraft and airship design. Volume I, Aircraft design

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Bibliographic Details
Main Author Nicolai, Leland M.
Other Authors Carichner, Grant
Format eBook
LanguageEnglish
Published Reston, VA : American Institute of Aeronautics and Astronautics, c2010.
SeriesAIAA education series.
Subjects
Online AccessFull text
ISBN9781613440469
Physical Description1 online zdroj (xxii, 883 p., 24 p. of plates) : ill. (some col.)

Cover

Table of Contents:
  • v. 1. Aircraft design. Introduction ; Review of practical aerodynamics ; Aircraft performance methods ; Aircraft operating envelope ; Preliminary estimate of takeoff weight ; Estimating the takeoff wing loading ; Selecting the planform and airfoil section ; Preliminary fuselage sizing and design ; High-lift devices ; Takeoff and landing analysis ; Preliminary sizing of the vertical and horizontal tails ; Designing for survivability (stealth) ; Estimating wing-body aerodynamics ; Propulsion system fundamentals ; Turbine engine inlet design ; Corrections for turbine engine installation ; Propeller propulsion systems ; Propulsion system thrust sizing ; Structures and materials ; Refined weight estimate ; Static stability and control ; Trim drag and maneuvering flight ; Control surface sizing criteria ; Life cycle cost ; Trade studies and sizing
  • Appendix A : Conversions
  • Appendix B : Atmospheric data
  • Appendix C : Isentropic compressible flow functions
  • Appendix D : Normal shock functions for a perfect gas
  • Appendix E : Plane oblique and conical shocks
  • Appendix F : NACA airfoil nomenclature and data
  • Appendix G : Aerodynamic data of real aircraft
  • Appendix H : Aerodynamics of wing-body combinations
  • Appendix I : Aircraft weights data
  • Appendix J : Propulsion data
  • Appendix K : Miscellaneous data.