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High Reynolds Number Subsonic Aerodynamics

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Release : 1970
Genre : Aerodynamics
Kind : eBook
Book Rating : /5 ( reviews)

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Book Synopsis High Reynolds Number Subsonic Aerodynamics by : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development

Download or read book High Reynolds Number Subsonic Aerodynamics written by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. This book was released on 1970. Available in PDF, EPUB and Kindle. Book excerpt:

Effects of Reynolds Number and Body Corner Radius on Aerodynamic Characteristics of a Space Shuttle-type Vehicle at Subsonic Mach Numbers

Download Effects of Reynolds Number and Body Corner Radius on Aerodynamic Characteristics of a Space Shuttle-type Vehicle at Subsonic Mach Numbers PDF Online Free

Author :
Release : 1972
Genre : Aerodynamics
Kind : eBook
Book Rating : /5 ( reviews)

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Book Synopsis Effects of Reynolds Number and Body Corner Radius on Aerodynamic Characteristics of a Space Shuttle-type Vehicle at Subsonic Mach Numbers by : Leland Howard Jorgenson

Download or read book Effects of Reynolds Number and Body Corner Radius on Aerodynamic Characteristics of a Space Shuttle-type Vehicle at Subsonic Mach Numbers written by Leland Howard Jorgenson. This book was released on 1972. Available in PDF, EPUB and Kindle. Book excerpt: 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.

High Reynolds Number Subsonic Aerodynamics

Download High Reynolds Number Subsonic Aerodynamics PDF Online Free

Author :
Release : 1970
Genre :
Kind : eBook
Book Rating : /5 ( reviews)

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Book Synopsis High Reynolds Number Subsonic Aerodynamics by : Rolland A. Willaume

Download or read book High Reynolds Number Subsonic Aerodynamics written by Rolland A. Willaume. This book was released on 1970. Available in PDF, EPUB and Kindle. Book excerpt: Contents: Advantages and problems of large subsonic aircraft; Aeromechanics; Scaling effects on shock-induced separation; Scaling effects on drag prediction; High Reynolds number subsonic aerodynamics; Advanced computer technology in aerodynamics; Engine performance considerations for the large subsonic transport; The aerodynamics of engine component design problems associated with large subsonic aircraft.

High Reynolds Number Subsonic Aerodynamics

Download High Reynolds Number Subsonic Aerodynamics PDF Online Free

Author :
Release : 1970
Genre : Aerodynamics
Kind : eBook
Book Rating : /5 ( reviews)

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Book Synopsis High Reynolds Number Subsonic Aerodynamics by : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development

Download or read book High Reynolds Number Subsonic Aerodynamics written by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. This book was released on 1970. Available in PDF, EPUB and Kindle. Book excerpt:

Subsonic Aerodynamics

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Author :
Release : 2003
Genre : Science
Kind : eBook
Book Rating : 306/5 ( reviews)

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Book Synopsis Subsonic Aerodynamics by : Ion Paraschivoiu

Download or read book Subsonic Aerodynamics written by Ion Paraschivoiu. This book was released on 2003. Available in PDF, EPUB and Kindle. Book excerpt:

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