George E. Kaattari, Jack N. Nielsen, William C. Pitts
This report is the second in a series investigating the effects of interference at supersonic speeds on the aerodynamic properties of wing-body combinations. The first report NACA RM A51J04, 1951, presented a method of determining the lift of triangular, rectangular, and trapezoidal wing-body combinations. The present report extends the same method to the determination of the pitching moments of these combinations.
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