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NACA0012 benchmark model using experimental flutter results with unsteady pressure distributions
1992
Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate)
M. N. Kogan1997
Assessment of dual-point drag reduction for an executive-jet modified airfoil section
Dennis O. Allison1996
Low-speed aerodynamic characteristics of a 1/8-scale X-29A airplane model at high angles of attack and side slip
Raymond D. Whipple1986