论文信息 - Buffet Tests of an Attack-airplane Model with Emphasis on Analysis of Data from Wind-tunnel Tests

Buffet Tests of an Attack-airplane Model with Emphasis on Analysis of Data from Wind-tunnel Tests

Memorandum presenting the buffet characteristics of a scale model of an attack airplane over a range of Mach numbers. The wing had a modified delta plan form with an NACA 0008 airfoil section at the root and an NACA 0005 airfoil section at the tip, a leading-edge sweep of 41.11 degrees, an aspect ratio of 2.91, and a taper ratio of 0.226. Results regarding the frequency spectrum of bending moment, effect of density on root-mean-square bending moment, system damping coefficients, and buffet input force are provided.

Dewey E Wornom | Don D Davis | D. D. Davis | D. Wornom

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