Author : Maxwell Alfred Heaslet
Publisher :
Page : 52 pages
File Size : 24,18 MB
Release : 1948
Category : Aerodynamics, Supersonic
ISBN :
A method is developed, consistent with the assumptions of small perturbation theory, which provides a means of determining for a known load distribution, the downwash behind a wing in supersonic flow. THe analysis is based upon the use of supersonic doublets which are distributed over the plan form and wake of the wing in a manner determined from the wing loading.
Author : Max A. Heaslet
Publisher :
Page : 726 pages
File Size : 39,84 MB
Release : 1948
Category : Aerodynamics, Supersonic
ISBN :
A method is developed, consistent with the assumptions of small perturbation theory, which provides a means of determining for a known load distribution, the downwash behind a wing in supersonic flow. THe analysis is based upon the use of supersonic doublets which are distributed over the plan form and wake of the wing in a manner determined from the wing loading.
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 1498 pages
File Size : 13,34 MB
Release : 1953
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 60 pages
File Size : 28,24 MB
Release : 1952
Category : Aeronautics
ISBN :
Author : S. S. Chin
Publisher :
Page : 304 pages
File Size : 13,56 MB
Release : 1961
Category : Guided missiles
ISBN :
Beskriver principperne i f.m. konstruktionen af styrede missiler.
Author : Douglas Godfrey
Publisher :
Page : 690 pages
File Size : 39,74 MB
Release : 1950
Category : Fretting corrosion
ISBN :
Fretting corrosion was concluded to be caused by the removal of finely divided and apparently virgin material due to inherent forces and that its primary reaction is independent of of vibratory motion or high sliding speeds. Fretting corrosion occurred to clean nonmetals and metals readily and glass microscope slides and steel balls provided an excellent method for visual studies.
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 498 pages
File Size : 40,82 MB
Release : 1952
Category : Aeronautics
ISBN :
Author : Dale E. Knutsen
Publisher :
Page : 72 pages
File Size : 33,81 MB
Release : 1968
Category : Airplanes
ISBN :
Author :
Publisher :
Page : 72 pages
File Size : 16,26 MB
Release : 19??
Category : Aerodynamics
ISBN :
Author : Harry E. Murray
Publisher :
Page : 744 pages
File Size : 26,77 MB
Release : 1950
Category : Laplace transformation
ISBN :
The lateral motions of aircraft are obtained by means of the Laplace transform which gives solutions in terms of elementary functions for the free motions and the motions due to forcing step functions. The lateral stability of a specific airplane and certain of its free and forced motions are calculated.
