Theoretical aerodynamic coefficients of two-dimensional supersonic biplanes

W. E. Moeckel
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.

An Adobe Acrobat (PDF) file of the entire report: