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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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User manual for computer program 55VD for computation of minimum induced drag and load distribution of nonplanar wings
Finite difference method for symmetric positive linear differential equations, discussing methods to solve finite difference equations generated
Unsteady two dimensional flow in square cavity with fluid initially at rest and constant velocity upper surface of cavity, noting vortex center
Scheme for choosing approximating system of difference equations for degenerate linear and nonlinear elliptic boundary value problems
Flow and pressure fields for spiral grooved pumping seal with specified groove dimensions and Reynolds number
Boundary conditions for Tricomi equation in symmetric positive form, showing analytical and finite difference solutions
Solution of differential equations by predictor corrector formulas for high order accuracy
Unsteady flow in two dimensional, rectangular cavity with upper wall moving
Flow fields construction for normal shock waves with nonequilibrium chemical reactions reflected from shock tube end wall
Nonlinear spinning shallow spherical shell equations solved for equilibrium stress and displacement distributions, discussing inertia loading
Discrete models for boundary value problems analysis in first strain-gradient elasticity theory, using extended finite element method
Viscous shock layer equations of laminar hypersonic flow past blunt body at moderate to high Reynolds numbers
Unsteady flow in rectangular cavity with moving wall, using iterative solution of Navier-Stokes equations
Mathematical model for impulsive heat releases by chemically generated waves in atmosphere
Green function in solving linear and nonlinear second order ordinary differential equations including examples in finding rendezvous and periodic orbits of restricted three body system
Computerized simulation of shock waves and flow fields behind supersonic edge delta wings and wing-body combinations
Development of computable electromagnetic theory model for lunar reflectivity problem - Vol. 3
One dimensional charged particle continuity equation solution in low energy neutral plasma with current flows