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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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Theoretical study of effect of pivot location on aerodynamic balance movement of variable sweep wings in incompressible flow
Method of integral relations applied to solution of incompressible turbulent boundary layer equations
Mathematical model for calculation of mean and fluctuating properties of incompressible turbulent boundary layers
Mixing length flow theory for analyzing incompressible turbulent swirling flow in pipes
Numerical techniques and solutions for compressible and incompressible laminar separated flows using time dependent finite difference equations
Similarity transformation and perturbation solution for laminar two dimensional incompressible jet flow over curved surface of small curvature
Stability of motions of incompressible materials with memory and relation to thermodynamic principles
Nonsimilar solution of incompressible turbulent boundary layer by integral matrix method
Rayleigh step journal bearings, considering pressure distribution, load capacity and attitude angle and optimal film thickness ratio for incompressible fluid lubrication
Incompressible laminar jet bounded by two parallel walls or by three walls, using linearized analysis related to Oseen approximation
Incompressible two dimensional turbulent boundary layer equations with arbitrary pressure distribution solved by weighted residual method
Unsteady laminar incompressible time dependent boundary layer flows with cylindrical symmetry, transverse boundaries and no swirl
Finite element method application to minimum principle for incompressible lubrication problem, noting flow boundary conditions and squeeze film effects
Conformal mapping technique yields linear, approximate solutions for calculating flow of an incompressible fluid through staggered array of cambered blades for the cases of flow with partial cavitation and supercavitation. Lift and drag coefficients, cavitation number, cavity shape, and exit flow conditions can be determined.
Rayleigh step journal bearings, considering pressure distribution, load capacity and attitude angle and optimal film thickness ratio for incompressible fluid lubrication
Integral relations method efficiency and accuracy in solving incompressible turbulent boundary layer equations, noting acceptability for turbulent flows with small wake components
Conservation equations for mass, mean momentum and kinetic energy for incompressible turbulent boundary layer, using finite difference procedure
Incompressible two dimensional turbulent boundary layer equations with arbitrary pressure distribution solved by weighted residual method