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  • Other Sources  (3)
  • 1980-1984
  • 1925-1929  (3)
  • 1926  (3)
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  • 1980-1984
  • 1925-1929  (3)
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  • 1
    Publication Date: 2019-06-28
    Description: This paper was delivered before the Royal Aeronautical Society as the 1925 Wilbur Wright Memorial lecture. It treats the subject of scale effect from the standpoint of the engineer rather than the physicist, in that it shows what compromises are necessary to secure satisfactory engineering model test data and how these test data compare with full scale or with theoretical values. The paper consists essentially of three parts: (1) a brief exposition of the theory of dynamic similarity, (2) application of the theory to airplane model tests, illustrated by test data on airfoils from the National Advisory Committee for Aeronautics variable-density wind tunnel, and (3) application of the theory to propeller testing, illustrated by comparisons of model and full-scale results.
    Type: NACA-TR-219
    Format: application/pdf
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  • 2
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    Unknown
    In:  CASI
    Publication Date: 2019-06-28
    Description: The most usual method of arriving at the maximum amount of spindling or hollowing out permissible in the case of any particular spar section is by trial and error, a process which is apt to become laborious in the absence of good guessing - or luck. The following tables have been got out with the object of making it possible to arrive with certainty at a suitable section at the first attempt.
    Type: NACA-TM-383
    Format: application/pdf
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  • 3
    facet.materialart.
    Unknown
    In:  CASI
    Publication Date: 2019-06-28
    Description: Certain principles are common to all metal spars and the design of a particular metal spar is followed throughout the design process.
    Type: NACA-TM-368
    Format: application/pdf
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