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Aerodynamic air foil surfaces for in-flight control for projectiles

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TLDR
Aerodynamical air foil surface and subsurface expressions and/or impressions of varied geometrics, angles of attack, heights and depths, comprising part of a projectile surface itself to create McClain effect molecular friction/pressure/temperature reaction flight control surfaces which automatically achieve in all fluids and velocities of flight self-stablizing spin and rotation, increased height of trajectory with corresponding enhancement of range and distance, kinetic energies, inducing smooth laminar boundary layer flows, substantially decreasing drag effects, synergistically combined to constitute a major technological improvement in performance of
Abstract
Aerodynamical air foil surface and subsurface expressions and/or impressions of varied geometrics, angles of attack, heights and depths, comprising part of a projectile surface itself to create McClain effect molecular friction/pressure/temperature reaction flight control surfaces which automatically achieve in all fluids and velocities of flight self-stablizing spin and rotation, increased height of trajectory with corresponding enhancement of range and distance, kinetic energies, inducing smooth laminar boundary layer flows, substantially decreasing drag effects, synergistically combined to constitute a major technological improvement in performance of all projectiles.

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References
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Double ramp discarding sabot

TL;DR: In this paper, a double ramp configuration and a centrally poioned obturating band in alignment with the center of gravity of an in-bore projectile were used to improve the uniformity of the shear traction forces at the interface between the sabot segments and a sub-caliber projectile, to reduce propellant gas blow-by and to enhance projectile inbore and trajectory stability.
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