Author : H. Hoene
Publisher :
Page : 740 pages
File Size : 48,20 MB
Release : 1951
Category : Equations of motion
ISBN :
The equations of motion for an airplane penetrating a gust are derived using a few simplifying assumptions. Calculations of loads for different static longitudinal stability on two German airplane models, HC 45 and HS 122, are compared with flight tests. Good agreement is obtained between the trend of the flight tests and the calculated values; however no absolute comparison was possible between the flight tests and calculations.
Author : Robert C. Nelson
Publisher :
Page : 464 pages
File Size : 34,4 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 : Thomas R. Yechout
Publisher : AIAA
Page : 666 pages
File Size : 46,51 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 : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 862 pages
File Size : 19,85 MB
Release : 1951
Category : Aeronautics
ISBN :
Author : Paul T. Hacker
Publisher :
Page : 650 pages
File Size : 38,39 MB
Release : 1951
Category : Airplanes
ISBN :
Data on the meteorological parameters pertinent to the aircraft icing problem are so summarized as to give the frequency of occurrence of observed icing situations according to two of the parameters. The summarized data indicate that statistical relations exist between some of the parameters. A method, based upon the collection efficiency of an airfoil and the frequency occurrence of icing situations with various liquid-water contents and mean-effective droplet sizes, is proposed for the selection of design criterions for ice-protection equipment. The method provides a convenient means of calculating the percenteage of icing encounters in which the water collection exceeds the design rate.
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 794 pages
File Size : 47,33 MB
Release : 1951
Category : Aeronautics
ISBN :
Chiefly translations from foreign aeronautical journals.
Author : Y C Fung
Publisher : Courier Dover Publications
Page : 516 pages
File Size : 48,49 MB
Release : 2008-10-17
Category : Technology & Engineering
ISBN : 0486469360
Geared toward advanced undergraduates and graduate students, this outstanding text surveys aeroelastic problems, their historical background, basic physical concepts, and the principles of analysis.
Author :
Publisher :
Page : 750 pages
File Size : 45,35 MB
Release : 1949
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 804 pages
File Size : 16,39 MB
Release : 1971
Category : Mechanics, Applied
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 274 pages
File Size : 11,61 MB
Release : 1953
Category : Aeronautics
ISBN :
