State Estimation Model Reduction Through the Manifold Boundary Approximation Method
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Magnetohydrodynamic boundary layer and heat transfer of a conducting fluid past a cylindrical body
Problems in computing transition matrices of lunar trajectories
Method which can be applied to the problem of an incompressible flow past an arbitrarily shaped cylindrical body in the presence of a magnetic field normal to the axis of the cylinder
Computation of transition matrices or error coefficients in midcourse guidance studies of lunar trajectories
Computation of transition matrices or error coefficients in midcourse guidance studies of lunar trajectories
Electromagnetic wave scattering by conducting cylinders with arbitrary cross sections - computation by point matching method
Synthesis and design of passive electric system realizing frequency patterns of transmission long line - designing nonreflecting four terminal amplifier with negative impedance
Pressure distributions prediction on blunt bodies at angle of attack, considering bodies of revolution and large angle cones
Newtonian fluid turbulent flow development characteristics in inlet region of smooth concentric annulus from momentum integral equations
Pressure distributions prediction on blunt bodies at angle of attack, considering bodies of revolution and large angle cones
The three-dimensional problem of transonic flow about lifting wing-body configurations is reduced to a two-variable computational problem with the method of matched asymptotic expansions. The computational problem is solved with the method of relaxation. The method accounts for leading-edge separation, the presence of shock waves, and the presence of solid, slotted, or porous tunnel walls. The Mach number range of the method extends from zero to the supersonic value at which the wing leading edge becomes sonic. A modified form of the transonic area rule which accounts for the effect of lift is developed. This effect is explained from simple physical considerations.
The handbook contains a set of curves that allow estimation of the average number of total daily delay minutes at a major airport under a variety of conditions. Demand profiles at each airport are classified with respect to the number of daily peak periods, the percentage of daily flights during peak periods, and the number of peak period operations at the airport. When combined with the saturation capacity of the airport, these descriptors provide sufficient information to allow usage of the handbook. Examples illustrating the use of the handbook are provided, as well as a brief review and description of the technical approach and of the computer package developed for this purpose.
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Previously cited in issue 13, p. 2109, Accession no. A82-30149
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