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Aerodynamic Forces On A Stationary And Oscillating Circular Cylinder At High Reynolds Numbers 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 Aerodynamic Forces On A Stationary And Oscillating Circular Cylinder At High Reynolds Numbers book. This book definitely worth reading, it is an incredibly well-written.
Author : G. W. Jones (Jr.)
Publisher : Unknown
Page : 74 pages
File Size : 55,5 Mb
Release : 1969
Category : Cylinders
ISBN : UIUC:30112106863514
Author : George W. Jones (Jr.)
Publisher : Unknown
Page : 76 pages
File Size : 54,8 Mb
Release : 1969
Category : Cylinders
ISBN : NASA:31769000423221
Author : George W. Jones (Jr.)
Publisher : Unknown
Page : 62 pages
File Size : 48,8 Mb
Release : 1969
Category : Cylinders
ISBN : OCLC:640949896
Author : Anonim
Publisher : Unknown
Page : 470 pages
File Size : 52,6 Mb
Release : 1977
Category : Aerodynamics
ISBN : MINN:31951000846665N
Author : Leland Howard Jorgenson,Jack J. Brownson
Publisher : Unknown
Page : 44 pages
File Size : 51,5 Mb
Release : 1972
Category : Aerodynamics
ISBN : UIUC:30112106883355
Static aerodynamic forces and moments were measured to study the effects of Reynolds number and body corner radius on the aerodynamic characteristics of a straight wing space shuttle orbiter at subsonic speeds. A 0.02-scale model was tested at Mach numbers from 0.3 to 0.9 and Reynolds numbers from about 600,000 to 3 million, based on body width. The body alone and the body with its wing and horizontal tail attached were tested at angles of attack from 35 to 75 degrees. The effects of rounding the body corners at the junctures connecting the bottom and sides were investigated for corner radii from 0 to 8.5 percent of the body width. At low subsonic Mach numbers (free stream Mach number approximately equal 0.3) the aerodynamic characteristics are affected significantly by changes in Reynolds number and body corner radius. With increase in Mach number to free stream Mach number = 0.9 the effect of Reynolds number seems to vanish, but a significant effect of body corner radius remains.
Author : S. Ziada,M. Samir,T. Staubli
Publisher : CRC Press
Page : 862 pages
File Size : 54,5 Mb
Release : 2000-01-01
Category : Science
ISBN : 9781482283747
Flow-induced vibrations and noise continue to cause problems in a wide range of engineering applications ranging from civil engineering and marine structures to power generation and chemical processing. These proceedings bring together more than a hundred papers dealing with a variety of topics relating to flow-induced vibration and noise. The cont
Author : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher : Unknown
Page : 962 pages
File Size : 51,8 Mb
Release : 1970
Category : Aeronautics
ISBN : CORNELL:31924057848867
Author : United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher : Unknown
Page : 966 pages
File Size : 52,5 Mb
Release : 1970
Category : Aeronautics
ISBN : STANFORD:36105113793769
Author : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher : Unknown
Page : 956 pages
File Size : 41,8 Mb
Release : 1970
Category : Science
ISBN : NASA:31769000659238
Author : Abrahim Lavi,T. Nejat Veziroğlu
Publisher : Unknown
Page : 606 pages
File Size : 46,6 Mb
Release : 1978
Category : Ocean thermal power plants
ISBN : UCSD:31822000631648
Author : Anonim
Publisher : Unknown
Page : 44 pages
File Size : 51,9 Mb
Release : 1984
Category : Aeronautics
ISBN : MINN:31951000845430J
Author : Wardlaw, Jr. (Andrew B.),Alfred Merle Morrison
Publisher : Unknown
Page : 52 pages
File Size : 50,7 Mb
Release : 1975
Category : Aerodynamic load
ISBN : UOM:39015095247162
Linear regression techniques are used to establish a quantitative description of side forces on bodies at high incidence. A data base is assembled concerning the key side force characteristics of maximum observed side force, angle of occurrence, and minimum angle of attack at which a side force is observed. This information is examined to determine the important trends and a predictive model for side force based on the crossflow analogy is developed to suggest other important variables. A linear regression model for these quantities is developed to include only those variables which are statistically significant. Results indicate that peak side force coefficients are a function of Mach number and only weakly of Reynolds number. Nose fineness is the critical model dimension which suggests that peak side force is a product of the nose flow field. The angle at which peak side forces occur is found to be dependent on model length and Mach number, while the onset angle of attack is a function of model length only.
Author : Lynn Faulkner,Jr., Earl Logan
Publisher : CRC Press
Page : 597 pages
File Size : 44,9 Mb
Release : 2000-12-14
Category : Technology & Engineering
ISBN : 9781482270372
Considering a broad range of fundamental factors and conditions influencing the optimal design and operation of machinery, the Handbook of Machinery Dynamics emphasizes the force and motion analysis of machine components in multiple applications. Containing details on basic theories and particular problems, the Handbook of Machinery Dynamics
Author : Arthur N. L. Chiu
Publisher : Unknown
Page : 392 pages
File Size : 44,5 Mb
Release : 1970
Category : Structural dynamics
ISBN : UCSD:31822001220300
Author : Anonim
Publisher : Unknown
Page : 780 pages
File Size : 46,8 Mb
Release : 1974
Category : Electronic
ISBN : MINN:31951000846519Y