Drag Due to Lift at Mach Numbers Up to 2.0
Author : Edward C. Polhamus
Publisher :
Page : 28 pages
File Size : 16,59 MB
Release : 1953
Category : Airplanes
ISBN :
Author : Edward C. Polhamus
Publisher :
Page : 28 pages
File Size : 16,59 MB
Release : 1953
Category : Airplanes
ISBN :
Author : Robert S. Osborne
Publisher :
Page : 20 pages
File Size : 11,42 MB
Release : 1953
Category : Airplanes
ISBN :
Author : Jon S. Pyle
Publisher :
Page : 36 pages
File Size : 49,39 MB
Release : 1971
Category : Drag (Aerodynamics)
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 936 pages
File Size : 28,79 MB
Release : 1948
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 166 pages
File Size : 34,74 MB
Release : 1992
Category : Science
ISBN :
Author : United States. National Aeronautics and Space Administration
Publisher :
Page : 164 pages
File Size : 31,3 MB
Release : 1989
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 836 pages
File Size : 38,8 MB
Release : 1977
Category :
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 988 pages
File Size : 18,45 MB
Release : 1950
Category : Aeronautics
ISBN :
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Author : Roelof Vos
Publisher : Springer
Page : 561 pages
File Size : 50,41 MB
Release : 2015-03-04
Category : Technology & Engineering
ISBN : 9401797471
Written to teach students the nature of transonic flow and its mathematical foundation, this book offers a much-needed introduction to transonic aerodynamics. The authors present a quantitative and qualitative assessment of subsonic, supersonic and transonic flow around bodies in two and three dimensions. The book reviews the governing equations and explores their applications and limitations as employed in modeling and computational fluid dynamics. Some concepts, such as shock and expansion theory, are examined from a numerical perspective. Others, including shock-boundary-layer interaction, are discussed from a qualitative point of view. The book includes 60 examples and more than 200 practice problems. The authors also offer analytical methods such as Method of Characteristics (MOC) that allow readers to practice with the subject matter. The result is a wealth of insight into transonic flow phenomena and their impact on aircraft design, including compressibility effects, shock and expansion waves, shock-boundary-layer interaction and aeroelasticity.
Author : H. Herbert Jackson
Publisher :
Page : 32 pages
File Size : 23,4 MB
Release : 1960
Category : Mach number
ISBN :