Author :
Publisher :
Page : 28 pages
File Size : 35,27 MB
Release : 1962
Category :
ISBN :
Author :
Publisher :
Page : 78 pages
File Size : 48,43 MB
Release : 1963
Category :
ISBN :
Author :
Publisher :
Page : 1492 pages
File Size : 29,20 MB
Release : 1966
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 1288 pages
File Size : 12,58 MB
Release : 1966-12
Category : Government publications
ISBN :
Author : Thomas R. Yechout
Publisher : AIAA
Page : 666 pages
File Size : 22,95 MB
Release : 2003
Category : Aerodynamics
ISBN : 9781600860782
Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.
Author :
Publisher :
Page : 236 pages
File Size : 17,29 MB
Release : 1979
Category :
ISBN :
Author : Robert C. Nelson
Publisher :
Page : 464 pages
File Size : 13,26 MB
Release : 1998
Category : History
ISBN :
This edition of this this flight stability and controls guide features an unintimidating math level, full coverage of terminology, and expanded discussions of classical to modern control theory and autopilot designs. Extensive examples, problems, and historical notes, make this concise book a vital addition to the engineer's library.
Author : Richard Eppler
Publisher : Springer Science & Business Media
Page : 569 pages
File Size : 41,24 MB
Release : 2012-12-06
Category : Technology & Engineering
ISBN : 3662026465
This detailed book describes a procedure for the design and analysis of subsonic airfoils. Contains 116 new airfoils for a wide range of Reynolds numbers and application requirements, including the input data for the computer code.
Author : Bernard Etkin
Publisher : John Wiley & Sons
Page : 392 pages
File Size : 23,24 MB
Release : 1982
Category : Technology & Engineering
ISBN :
Author : Ira H. Abbott
Publisher : Courier Corporation
Page : 708 pages
File Size : 13,38 MB
Release : 2012-04-26
Category : Technology & Engineering
ISBN : 0486134997
Concise compilation of subsonic aerodynamic characteristics of NACA wing sections, plus description of theory. 350 pages of tables.
