Aerodynamic Characteristics of Non-straight-taper Wings
Author : David B. Benepe
Publisher :
Page : 322 pages
File Size : 13,1 MB
Release : 1966
Category : Airplanes
ISBN :
Author : David B. Benepe
Publisher :
Page : 322 pages
File Size : 13,1 MB
Release : 1966
Category : Airplanes
ISBN :
Author : C. W. Smith
Publisher :
Page : 152 pages
File Size : 12,82 MB
Release : 1979
Category :
ISBN :
Author : Defense Documentation Center (U.S.)
Publisher :
Page : 784 pages
File Size : 26,68 MB
Release : 1967
Category : Science
ISBN :
Author :
Publisher :
Page : 152 pages
File Size : 27,60 MB
Release : 1979
Category : Aerodynamics
ISBN :
Author :
Publisher :
Page : 478 pages
File Size : 29,98 MB
Release : 1970
Category :
ISBN :
Author : E. Torenbeek
Publisher : Springer Science & Business Media
Page : 607 pages
File Size : 24,20 MB
Release : 2013-06-29
Category : Technology & Engineering
ISBN : 9401732027
Since the education of aeronautical engineers at Delft University of Technology started in 1940 under tae inspiring leadership of Professor H.J. van der Maas, much emphasis has been placed on the design of aircraft as part of the student's curriculum. Not only is aircraft design an optional subject for thesis work, but every aeronautical student has to carry out a preliminary airplane design in the course of his study. The main purpose of this preliminary design work is to enable the student to synthesize the knowledge ob tained separately in courses on aerodynamics, aircraft performances, stability and con trol, aircraft structures, etc. The student's exercises in preliminary design have been directed through the years by a number of staff members of the Department of Aerospace Engineering in Delft. The author of this book, Mr. E. Torenbeek, has made a large contribution to this part of the study programme for many years. Not only has he acquired vast experience in teaching airplane design at university level, but he has also been deeply involved in design-oriented re search, e.g. developing rational design methods and systematizing design information. I am very pleased that this wealth of experience, methods and data is now presented in this book.
Author : Harry E. Murray
Publisher :
Page : 744 pages
File Size : 20,29 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.
Author : Abe Silverstein
Publisher :
Page : 76 pages
File Size : 47,70 MB
Release : 1937
Category : Aerofoils
ISBN :
Author : M. I. Goldhammer
Publisher :
Page : 262 pages
File Size : 44,30 MB
Release : 1973
Category : Short take-off and landing aircraft
ISBN :
This volume describes engineering methods for the prediction of the aerodynamic and stability and control characteristics of STOL aircraft employing internally ducted jet flaps, externally blown jet flaps, and mechanical flap systems with vectored thrust. These methods are intended to be used in conjunction with the theoretical methods and the associated computer program (STOL Aerodynamic Methods Computer Program) discussed in Volumes I and II, respectively. These engineering methods are intended to provide a rational approach for the aerodynamic analysis of complete STOL aircraft configurations and to provide semi-empirical methods to account for those effects not treated by the theoretical methods. These methods have been applied to configurations representative of each of the powered high-lift concepts, and the results of these analyses have been presented along with available experimental data to indicate the validity and range of applicability of the methods.
Author :
Publisher :
Page : 1006 pages
File Size : 19,40 MB
Release : 1960
Category : Mechanics, Applied
ISBN :