The Determination of Span Load Distribution at High Speeds by Use of High-Speed Wind-Tunnel Section Data
Description:
Report presenting a tabular method for determining the span load distribution at high Mach numbers by utilizing high-speed airfoil section data. This method, which is also called the generalized method, is an easily applied process of successive approximations by which a general application of the lifting-line theory may be used to determine the span load distribution for wings composed of sections with arbitrary lift curves. An example is provided to show how the method is used.
Date:
February 1944
Creator:
Boshar, John
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department