Experimental Pressure Distributions Over Wing Tips at Mach Number 1.9

Released on by Harold Mirels
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  • Experimental Pressure Distributions Over Wing Tips at Mach Number 1.9 Book Detail

  • Author : Harold Mirels
  • Release Date : 1949
  • Publisher :
  • Genre : Aerodynamic load
  • Pages : 28
  • ISBN 13 :
  • File Size : 86,86 MB
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Experimental Pressure Distributions Over Wing Tips at Mach Number 1.9 by Harold Mirels PDF Summary

Book Description: An investigation was conducted at a Mach number of 1.90 to determine spanwise pressure distribution over a wing tip in a region influenced by a sharp subsonic trailing edge. The wing section was a symmetrical wedge of 5 degrees 43 minutes total included angle in the free-stream direction. The investigation was conducted over a range of angles of attack from -10 to 10 degrees at a Reynolds number of 3,400,000 per foot.

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