A Wind tunnel Investigation of Three Propellers Through an Angle of attack Range from 0 Degree to 85 Degrees Book [PDF] Download

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Detail About A Wind tunnel Investigation of Three Propellers Through an Angle of attack Range from 0 Degree to 85 Degrees PDF

  • Author : Paul F. Yaggy
  • Publisher : Anonim
  • Genre : Propellers, Aerial
  • Total Pages : 86 pages
  • ISBN :
  • PDF File Size : 41,9 Mb
  • Language : English
  • Rating : 4/5 from 21 reviews

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NASA SP.

NASA SP.
  • Publisher : Unknown Publisher
  • File Size : 54,5 Mb
  • Release Date : 29 April 1986
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Aeronautical Engineering

Aeronautical Engineering
  • Publisher : Unknown Publisher
  • File Size : 49,7 Mb
  • Release Date : 29 April 1986
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A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (

Wind-tunnel Investigation of Effect of Sweep on Rolling Derivatives at Angles of Attack Up to 13© and at High Subsonic Mach Numbers, Including a Semiempirical Method of Estimating the Rolling Derivatives

Wind-tunnel Investigation of Effect of Sweep on Rolling Derivatives at Angles of Attack Up to 13© and at High Subsonic Mach Numbers, Including a Semiempirical Method of Estimating the Rolling Derivatives
  • Publisher : Unknown Publisher
  • File Size : 28,7 Mb
  • Release Date : 29 April 2024
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An investigation was performed in the Langley high-speed 7- by 10-foot tunnel in order to determine the rolling derivatives for swept-wing-body configurations at angles of attack from 0 degrees to 13 degrees