Author : Max A. Heaslet
Publisher :
Page : 726 pages
File Size : 28,11 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 : Harvard Lomax
Publisher :
Page : 19 pages
File Size : 27,97 MB
Release : 1950
Category : Aeronautics
ISBN :
Author : Maxwell Alfred Heaslet
Publisher :
Page : 52 pages
File Size : 34,14 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 : 19 pages
File Size : 34,96 MB
Release : 1950
Category :
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 1038 pages
File Size : 13,24 MB
Release : 1956
Category : Aeronautics
ISBN :
Author : Eugene S. Love
Publisher :
Page : 702 pages
File Size : 25,11 MB
Release : 1955
Category : Aerodynamic load
ISBN :
Some recent contributions to the problem of shock-induced separation of the boundary layer are examined, and additional analytical and experimental results are presented. The probable ranges of pressure rises and flow deflections associated with separation are indicated. Consideration is given to the effects of Mach number, adverse pressure gradient, and Reynolds number for laminar boundary layers and to the effects of Mach number, Reynolds number, and ratio of sepcific heats for turbulent boundary layers.
Author :
Publisher :
Page : 388 pages
File Size : 49,52 MB
Release : 1948
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 60 pages
File Size : 41,13 MB
Release : 1952
Category : Aeronautics
ISBN :
Author : S. S. Chin
Publisher :
Page : 304 pages
File Size : 46,83 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 : 44,72 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.
