A simple empirical formulation of electron emission from cesiated metal surfaces
Empirical converter surface physics formulation for electron emission current density analysis on cesiated metal surface
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Empirical converter surface physics formulation for electron emission current density analysis on cesiated metal surface
Analytic formulation of three wedge angle constraints in trajectory studies
Discrete models formulated for thermomechanical behavior of materials with memory, obtaining equations of motion and heat conduction for finite elements of nonlinear continua
Semi-Lagrangian formulation of Vlasov equation in two and three dimensional electrostatic problems, investigating tensor determinants and perturbation
Integral equation formulations for electromagnetic scattering from two-dimensional inhomogeneities in conductive earth
Integral equation formulations for electromagnetic scattering from two-dimensional inhomogeneities in conductive earth - appendices, figures, bibliography, and computer programs
Formulation of design rules for PCM telemetry frame synchronization
Perturbation theory using variation of parameters formulation to calculate satellite orbits
Mathematical formulation of Double Precision Orbit Determination Program /DPODP/ for lunar and planetary mission spacecraft trajectories
Electron emission formulation for cesiated metal surfaces in thermionic converter in terms of work function, using Swanson-Strayer correlation
Canonical perturbation theory formulation applied to Poincare-von Zeipel method
Low modulus solid propellants family for low thrust-to-mass ratio fully case bonded end-burning motors, using polymer network theory for binder formulation
Continuous media nonlinear thermomechanical behavior, presenting finite element formulation of deformation and irreversible thermodynamics problems
Active network analysis by topological formulation, eliminating k-trees
Nonlinear static structural mechanical problems solution, using self correcting initial value formulations
A mathematical model and computer program were implemented to study the main rotor free wake geometry effects on helicopter rotor blade air loads and response in steady maneuvers. The theoretical formulation and analysis of results are presented.
A general theory of elastoplastic flow is formulated for work-hardening materials that may be both anisotropic and compressible. Because the theory is quasi-linear, it may be cast in terms of integral equations and the result is an extended form of Somigliana's identity. When these relations are evaluated on the boundary of a solid, their dimensionality is reduced. Previous experience with simpler materials shows that arbitrary problems may be solved in a direct manner.
The use of metric tensors as inputs to computer programs designed to formulate engineering and scientific problems is considered as an alternative to the use of coordinate transformation equations.