Low-speed Aerodynamic Characteristics of a 1
Author : Raymond D. Whipple
Publisher :
Page : pages
File Size : 41,89 MB
Release : 1986
Category :
ISBN :
Author : Raymond D. Whipple
Publisher :
Page : pages
File Size : 41,89 MB
Release : 1986
Category :
ISBN :
Author : Robert J. McGhee
Publisher :
Page : 92 pages
File Size : 22,46 MB
Release : 1980
Category : Aerodynamics
ISBN :
Wind tunnel tests were conducted to determine the low speed two dimensional aerodynamic characteristics of a 17 percent thick medium speed airfoil (MS(1)-0317) designed for general aviation applications. The results were compared with data for the 17 percent thick low speed airfoil (LS(1)-0417) and the 13 percent thick medium speed airfoil (MS(1)-0313). Theoretical predictions of the drag rise characteristics of this airfoil are also provided. The tests were conducted in the Langley low turbulence pressure tunnel over a Mach number range from 0.10 to 0.32, a chord Reynolds number range from 2 million to 12 million, and an angle of attack range from about -8 to 20 deg.
Author : Charles L. Ladson
Publisher :
Page : 104 pages
File Size : 19,87 MB
Release : 1988
Category : Aerofoils
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Author : William D. Beasley
Publisher :
Page : 74 pages
File Size : 48,57 MB
Release : 1975
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Author : Edward Charles Polhamus
Publisher :
Page : 32 pages
File Size : 47,78 MB
Release : 1959
Category : Cylinders
ISBN :
Author : James S. Bowman
Publisher :
Page : 66 pages
File Size : 41,68 MB
Release : 1960
Category : Aerodynamics
ISBN :
Author : Michael S. Selig
Publisher : Soartech
Page : 320 pages
File Size : 20,22 MB
Release : 1995
Category : Technology & Engineering
ISBN :
Author : Daniel W. Banks
Publisher :
Page : 348 pages
File Size : 16,22 MB
Release : 1992
Category : Aerodynamics
ISBN :
Author : R. J. McGhee
Publisher :
Page : 88 pages
File Size : 17,30 MB
Release : 1979
Category :
ISBN :
Author : Williams J. Alford
Publisher :
Page : 30 pages
File Size : 22,87 MB
Release : 1959
Category : Aerodynamics
ISBN :