Transonic flow in a converging-diverging nozzle Final report
Computerized solutions to finite difference equations of motion of transonic flow in converging-diverging rocket nozzles
Prozan, R. J.↗
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Results for “finite difference”
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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Low gravity draining from hemispherically bottomed cylindrical tanks Final report
Finite difference model of low gravity draining of inviscid incompressible liquids from cylindrical tanks with hemispherical bottoms
Bizzell, G. D.↗
Calculation of mean and fluctuating properties of the incompressible turbulent boundary layer
Conservation equations for mass, mean momentum and kinetic energy for incompressible turbulent boundary layer, using finite difference procedure
Beckwith, I. E.↗
Axisymmetric static and dynamic buckling of spherical caps due to centrally distributed pressures
Spherical caps axisymmetric static and dynamic buckling under load, using axisymmetric nonlinear elastic shell theory approximation and finite difference equations
Fulton, R. E.↗
Numerical solutions of laminar separated flows
Numerical techniques and solutions for compressible and incompressible laminar separated flows using time dependent finite difference equations
Mueller, T. J.↗
Numerical integration of products of Fourier and ordinary polynomials
Coefficients for finite difference methods of numerical integration of products of Fourier and ordinary polynomials
Bettis, D. G.↗
A time integration method for computation of the intensities of seismic rays
Finite difference time integration method for computing seismic ray intensities
Wesson, R. L.↗
Calculation of nonequilibrium hypersonic turbulent boundary layers and comparisons with experimental data
Compressible hypersonic turbulent boundary layers solution by finite difference method, relating mixing length to velocity profile shape factor
Beckwith, I. E.↗
Numerical methods for mixed boundary value problems of shells of revolution
Numerical methods for mixed boundary value problem of axisymmetric shells of revolution, using truncated series expansion and finite difference expressions
Kalnins, A.↗
Stress, buckling, and vibration analysis of shells of revolution
Stress, buckling and vibration analysis of shells of revolution by numerical integration and finite difference methods, summarizing computer programs
Anderson, M. S.↗
Radiation view factor program
Computer program, RAVFAC, calculates diffuse radiation view factors, using contour integrals. Technique is combined with finite difference /double summation/ technique to compose total program package.
Lovin, J. K.↗
Computer program calculates transonic velocities in turbomachines
Computer program, TSONIC, combines velocity gradient and finite difference methods to obtain numerical solution for ideal, transonic, compressible flow for axial, radial, or mixed flow cascade of turbomachinery blades.
Katsanis, T.↗
The compressible turbulent boundary layer on a blunt swept slab with and without leading- edge blowing
Finite difference method for solving equations for compressible turbulent boundary layers on swept infinite cylinders
Beckwith, I. E.↗
A computational method for unified solutions to the inviscid flow field about blunt bodies
Finite difference method for unified solutions to inviscid supersonic flow distribution about blunt bodies
Aungier, R. H.↗
Thermal buckling analysis for stiffened orthotropic cylindrical shells
Structural analysis of thermal buckling of orthotropic, multilayered, stiffened cylindrical shell using finite differences and determinant plotting or modal iteration
Card, M. F.↗
A numerical procedure to calculate the inviscid flow field about a space shuttle orbiter traveling at a supersonic/hypersonic velocity
Finite difference method for calculating inviscid flow field around supersonic/hypersonic space shuttle
Grossman, B.↗
A time-dependent method for calculating supersonic angle-of-attack flow about axisymmetric blunt bodies with sharp shoulders and smooth nonaxisymmetric blunt bodies
Hypersonic and supersonic angle of attack flow about asymmetric and axisymmetric blunt bodies based on time dependent finite difference theory and method of characteristics
Barnwell, R. W.↗
Modified thermal analyzer digital computer program (TAP)
Computer program for solving n-dimensional transient or steady state heat flow problems by creating electrical analogy of problem and solving by finite difference method
Knittle, D. E.↗