Author : Carl R. Huss
Publisher :
Page : 28 pages
File Size : 50,95 MB
Release : 1959
Category : Airplanes
ISBN :
A study of the effect of the frequency of the lowest wing structural mode on the airplane center-of-gravity dynamic-response factor was made by employing simplified transfer functions. It was found that the simplified transfer function adequately predicted the maximum value of the incremental normal-load-factor response at the airplane center of gravity to isosceles triangle pulse elevator inputs.
Author :
Publisher :
Page : 20 pages
File Size : 46,22 MB
Release : 1959
Category : Airplanes
ISBN :
Author : James J. Donegan
Publisher :
Page : 20 pages
File Size : 24,65 MB
Release : 1959
Category :
ISBN :
Author : Henry A. Cole (Jr.)
Publisher :
Page : 74 pages
File Size : 41,28 MB
Release : 1954
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 966 pages
File Size : 13,65 MB
Release : 1958
Category : Aeronautics
ISBN :
Author : United States. National Aeronautics and Space Administration
Publisher :
Page : 500 pages
File Size : 48,55 MB
Release : 1959
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 494 pages
File Size : 26,80 MB
Release : 1959
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 388 pages
File Size : 42,29 MB
Release : 1957
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 388 pages
File Size : 30,4 MB
Release : 1959
Category : Aeronautics
ISBN :
Author : United States. National Aeronautics and Space Administration
Publisher :
Page : 300 pages
File Size : 47,56 MB
Release : 1960
Category :
ISBN :
