Author : Royce L. McKinney
Publisher :
Page : 52 pages
File Size : 30,36 MB
Release : 1965
Category : Aerodynamic load
ISBN :
Author : Maurice O. Feryn
Publisher :
Page : 36 pages
File Size : 37,49 MB
Release : 1966
Category :
ISBN :
Author :
Publisher :
Page : 52 pages
File Size : 35,12 MB
Release : 1965
Category :
ISBN :
Author : Lloyd S. Jernell
Publisher :
Page : 74 pages
File Size : 41,27 MB
Release : 1965
Category : Aerodynamic load
ISBN :
Author :
Publisher :
Page : 36 pages
File Size : 43,67 MB
Release : 1966
Category :
ISBN :
Author : Albert G. Few
Publisher :
Page : 80 pages
File Size : 19,85 MB
Release : 1954
Category : Airplanes
ISBN :
The drag due to lift increases with increasing sweep through the Mach number range. Some increase in bag due to lift is evident decrease in taper ratio for wings having 300of sweep through most of the speed range.
Author : Allen B. Henning
Publisher :
Page : 32 pages
File Size : 49,67 MB
Release : 1957
Category : Aerofoils
ISBN :
An investigation was made to determine the effects of wing inboard plan-form modifications on the lift, drag, and longitudinal characteristics of a rocket-propelled free-flight model. The model had a body of fineness ration 17.4, a modified wing with a basic plan form swept back 52.5 degrees and an aspect ratio of 3, and inline horizontal tail surfaces which were aerodynamically pulsed continuously throughout the flight.
Author : Maurice O. Feryn
Publisher :
Page : 66 pages
File Size : 39,65 MB
Release : 1965
Category : Airframes
ISBN :
Author :
Publisher :
Page : 768 pages
File Size : 28,54 MB
Release : 1963
Category : Science
ISBN :
Author :
Publisher :
Page : 34 pages
File Size : 16,33 MB
Release : 1983
Category :
ISBN :
