Download Full eBooks in PDF
Analysis Of The Linearized Supersonic Flow About Pointed Bodies Of Revolution By The Method Of Characteristics Book in PDF, ePub and Kindle version is available to download in english. Read online anytime anywhere directly from your device. Click on the download button below to get a free pdf file of Analysis Of The Linearized Supersonic Flow About Pointed Bodies Of Revolution By The Method Of Characteristics book. This book definitely worth reading, it is an incredibly well-written.
Author : Alan D. Sherer
Publisher : Unknown
Page : 52 pages
File Size : 50,6 Mb
Release : 1966
Category : Aerodynamics, Supersonic
ISBN : UIUC:30112106686865
Author : Anonim
Publisher : Unknown
Page : 628 pages
File Size : 41,9 Mb
Release : 1966
Category : Electronic
ISBN : MINN:31951000846026L
Author : Anonim
Publisher : Unknown
Page : 528 pages
File Size : 40,8 Mb
Release : 1973
Category : Mechanics, Applied
ISBN : UCAL:C2682442
Author : United States. Superintendent of Documents
Publisher : Unknown
Page : 1348 pages
File Size : 51,9 Mb
Release : 1970
Category : United States
ISBN : STANFORD:36105019598304
Author : United States. Superintendent of Documents
Publisher : Unknown
Page : 1248 pages
File Size : 53,7 Mb
Release : 1961
Category : Government publications
ISBN : WISC:89038149167
Author : United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher : Unknown
Page : 2300 pages
File Size : 41,7 Mb
Release : 1967
Category : Aeronautics
ISBN : STANFORD:36105113793777
Author : Anonim
Publisher : Unknown
Page : 750 pages
File Size : 44,8 Mb
Release : 1949
Category : Aeronautics
ISBN : UVA:X004173285
Author : Anonim
Publisher : Unknown
Page : 1466 pages
File Size : 44,8 Mb
Release : 1966
Category : Government publications
ISBN : MINN:319510005782185
Author : Anonim
Publisher : Unknown
Page : 590 pages
File Size : 52,6 Mb
Release : 1992
Category : Aeronautics
ISBN : MINN:31951P00231912Z
Author : Anonim
Publisher : Unknown
Page : 748 pages
File Size : 49,5 Mb
Release : 1963
Category : Aeronautics
ISBN : STANFORD:36105024827888
Author : Library of Congress. Science and Technology Division
Publisher : Unknown
Page : 1196 pages
File Size : 46,8 Mb
Release : 1961
Category : Military research
ISBN : OSU:32435051670529
Author : William Perl,Milton M. Klein
Publisher : Unknown
Page : 724 pages
File Size : 44,8 Mb
Release : 1950
Category : Air flow
ISBN : STANFORD:36105024796059
The transonic similarity law for two-dimensional flow derived by von Karman was investigated by an iteration procedure similar to that of the Rayleigh-Janzen and Ackeret-Prandtl-Glauert methods. The results, which show that the potential can be expressed as a power series in a single parameter that depends on Mach number, thickness ratio, and ratio of specific heats, are in agreement with those of von Karman. By the iteration procedure, the second approximation for the flow past a Kaplan section was obtained in similarity form. The exact solution by Kaplan for the second approximation was examined and found expressible in the same similarity form. The exact numerical results to three approximations obtained by Kaplan for the Kaplan section and the circular arc have been reduced to transonic similarity form.
Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 1110 pages
File Size : 50,9 Mb
Release : 1951
Category : Aeronautics
ISBN : RUTGERS:39030037542240
Author : Allen F. Donovan
Publisher : Princeton University Press
Page : 863 pages
File Size : 52,5 Mb
Release : 2015-12-08
Category : Science
ISBN : 9781400879908
Volume VII of the High Speed Aerodynamics and Jet Propulsion series. It deals with applications to specific components of the complete aircraft. Sections of the volume include: aerodynamics of wings at high speed, aerodynamics of bodies at high speed, interaction problems, propellers at high speed, diffusers and nozzles, and nonsteady wing characteristics. Originally published in 1957. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
Author : Paul T. Hacker,Robert G. Dorsch
Publisher : Unknown
Page : 650 pages
File Size : 44,9 Mb
Release : 1951
Category : Airplanes
ISBN : STANFORD:36105024831153
Data on the meteorological parameters pertinent to the aircraft icing problem are so summarized as to give the frequency of occurrence of observed icing situations according to two of the parameters. The summarized data indicate that statistical relations exist between some of the parameters. A method, based upon the collection efficiency of an airfoil and the frequency occurrence of icing situations with various liquid-water contents and mean-effective droplet sizes, is proposed for the selection of design criterions for ice-protection equipment. The method provides a convenient means of calculating the percenteage of icing encounters in which the water collection exceeds the design rate.