Book Description
Numerical calculations of the paths of water drops in an air stream around a circular cylinder are given. From these calculations, information is obtained on the percentage of the swept area cleared of drops.
Author : Arthur Kantrowitz
Publisher :
Page : 22 pages
File Size : 23,77 MB
Release : 1940
Category : Aerodynamic heating
ISBN :
Numerical calculations of the paths of water drops in an air stream around a circular cylinder are given. From these calculations, information is obtained on the percentage of the swept area cleared of drops.
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 596 pages
File Size : 16,88 MB
Release :
Category : Aeronautics
ISBN :
Author : William Lewis
Publisher :
Page : 536 pages
File Size : 36,16 MB
Release : 1947
Category : Aeronautics
ISBN :
Data from flight measurements of the meteorological factors related to the intensity of icing conditions are presented. The physical factors that establish the distribution of liquid water in clouds of various types are discussed and the results of the analysis are used to formulate certain rules for the forecasting of icing intensity. The problems of determining the range of values of the significant factors defining icing intensity for the purpose of the design of ice-protection equipment are discussed and tentative values are given.
Author : E. R. G. Eckert
Publisher :
Page : 330 pages
File Size : 27,79 MB
Release : 1955
Category : Aerodynamics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 634 pages
File Size : 28,51 MB
Release :
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 98 pages
File Size : 44,30 MB
Release : 1943
Category : Aeronautics
ISBN :
Author : F. L. Thompson
Publisher :
Page : 566 pages
File Size : 26,85 MB
Release : 1940
Category : Airplanes
ISBN :
It may be concluded that the stalling of vertical tail surfaces is not in itself a dangerous condition. Provided sufficient directional stability exists at large angles of sideslip, the tail stall may occur with modern airplanes, as with those of the past, without the knowledge of or concern to the pilot.
Author :
Publisher :
Page : 412 pages
File Size : 37,97 MB
Release : 1948
Category : Aeronautics
ISBN :
Author : Albert J. Evans
Publisher :
Page : 326 pages
File Size : 15,84 MB
Release : 1953
Category : Aerodynamic load
ISBN :
Author :
Publisher :
Page : 1718 pages
File Size : 36,53 MB
Release : 1946
Category : Government publications
ISBN :