Full-Scale Investigation of an Equilateral Triangular Wing Having 10-Percent-Thick Biconvex Airfoil Sections Page: 3 of 36
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NACA RM No. L8GO
Figure 1.- The stability system of axes an sign convention for the
standard. NACA coefficients. All forces , force coefficients, moment
coefficients, angles, and control-surface deflections are shown as
w f ,
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Whittle, Edward F., Jr. & Lovell, J. Calvin. Full-Scale Investigation of an Equilateral Triangular Wing Having 10-Percent-Thick Biconvex Airfoil Sections, report, September 30, 1948; (digital.library.unt.edu/ark:/67531/metadc64596/m1/3/: accessed January 20, 2019), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.