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A numerical study of a laminar, compressible boundary layer about an airfoil
The primary goal of this study is to develop a finite element method for the calculation of an attached, two-dimensional, laminar, compressible boundary layer about an air-foil in a subsonic free stream. An introduction ...
The effect of lift on aeroassisted orbital transfer trajectories
Miele, Wang, and Deaton have demonstrated in Ref. 1 how optimal trajectories are produced by eliminating positive lift and fixing the lift coefficient at its lower, negative (downward) bound all throughout the atmospheric ...