Theoretical aerodynamic coefficients of two-dimensional supersonic biplanes

W. E. Moeckel
naca-tn-1316
Jun 1947


The effect of varying the design of supersonic biplanes has been theoretically investigated to determine the configuration required for optimum aerodynamic performance. The investigation was chiefly concerned with biplanes having lower and upper airfoils of equal chord length and of triangular cross section.

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