Maximum lift-to-drag ratio of a slender, flat-top, hypersonic body.
Lift-drag ratio attainable by slender flat-top body at supersonic speeds, considering Newtonian pressure distribution and constant skin friction
Engineering topics
Publications and source records attributed to Miele, A..
Lift-drag ratio attainable by slender flat-top body at supersonic speeds, considering Newtonian pressure distribution and constant skin friction
Maximum lift-drag ratio of slender, flat top, hypersonic body assuming modified Newtonian pressure distribution and constant surface averaged skin friction coefficient
Optimization of lift drag ratio of lifting bodies at hypersonic speeds
Lift to drag ratios of slender, conical bodies flying at hypersonic speeds, and effects of geometric parameters on aerodynamic stability
Optimum hypersonic lifting wings
Optimum shaped-bodies of maximum lift-to-drag ratio in hypersonic flow for modified Newtonian pressure distribution and constant skin friction
Three-dimensional slender wings of maximum lift/ drag ratio in hypersonic flow studied by variational calculus under several lift and volume conditions
Similarity laws for bodies maximizing lift-to-drag ratio at hypersonic speeds, considering longitudinal and transversal contours
Lift-to-drag ratio attainable by slender, homothetic body at hypersonic speeds, assuming Newtonian pressure distribution and constant skin-friction coefficient
Lift-drag ratios of slender, affine wings at hypersonic speeds
One-dimensional approach to maximum lift-drag ratio of slender, flat-top, affine wing at hypersonic speeds
Two-dimensional approach to maximum lift-drag ratio of slender, flat-top, wing at hypersonic speeds
Similarity laws for determining chordwise and spanwise contours minimizing drag of flat-top wing in hypersonic flow
Maximizing lift-drag ratio of slender, flat-top, hypersonic body assuming Newtonian pressure distribution and constant skin-friction coefficient
Lift-drag ratios analyzed for lifting wings in hypersonic flow
Three-dimensional lifting wings of minimum drag in hypersonic flow
Optimizing lift-to-drag ratio of slender, flat-top wing of given planform in hypersonic flow by using variational calculus methods
Maximizing lift-to-drag ratio of slender body in hypersonic flow investigated by calculus of variations