Orderly three-dimensional processes in turbulent boundary layers on ablating bodies
Flow model for three dimensional processes in turbulent boundary layers of ablating hypersonic Plexiglas bodies
Canning, T. N.↗
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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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Newtonian aerodynamics for general surfaces.
Newtonian flow model, calculating hypersonic reentry aerodynamic forces for complicated body shapes
Heybey, W. H.↗
An analytical study of separated flow about circular cylinders.
Lift and drag coefficients for circular cylinder immersed in time dependent flow analyzed using potential flow model
Sarpkaya, T.↗
Perturbations of the interplanetary magnetic field by the lunar wake.
Interplanetary magnetic field perturbations by lunar wake using plasma flow model
Behannon, K. W.↗
Creeping flow solution of Leidenfrost boiling with a moving surface.
Creeping flow model of Leidenfrost boiling with moving surface, discussing vaporization time for equivalent drop film boiling on stationary surface
Baumeister, K. J.↗
Theoretical study of vortex shedding from bodies of revolution undergoing coning motion
Flow model for vortex shedding from slender body in coning motion
Kuhn, G. D.↗
An analytical study of separated flow about circular cylinders.
Lift and drag coefficients for circular cylinder immersed in time dependent flow analyzed using potential flow model
Sarpkaya, T.↗
Creeping flow solution of Leidenfrost boiling with a moving surface.
Creeping flow model of Leidenfrost boiling with moving surface, discussing vaporization time for equivalent drop film boiling on stationary surface
Baumeister, K. J.↗
Survey of the relationship between theory and experiment for convective heat transfer from rocket combustion gases.
Compressible turbulent accelerating boundary layer flow model for convective heat transfer from rocket combustion gases, noting heat flux
Bartz, D. R.↗
Hydromagnetic waves - Theory and applications.
Hydromagnetic waves equations of motion for nonrelativistic case, discussing particle and fluid flow models
Kanwal, R. P.↗
Calculation of jet interference effects on V/STOL aircraft by a nonplanar potential flow method
Potential flow model for calculating jet interference effects on V/STOL aircraft
Rubbert, P. E.↗
A correlation of subcooled-boiling pressure drop for low-pressure water flowing in tubes with constant heat flux
One dimensional flow model to correlate subcooled boiling pressure drop in circular tubes with constant heat flux
Stone, J. R.↗
A long wave approximation to peristaltic motion
Peristaltic motion of viscous incompressible fluid, applying long wave approximation to two dimensional urine flow model
Ostrach, S.↗
Recompression of a two dimensional supersonic turbulent free shear layer
Flow model for recompression of two dimensional supersonic turbulent free shear layer
Chow, W. L.↗
An analytical and experimental study of nonuniform plug nozzle flow fields
Nonuniform plug nozzle flow field calculated for closed wake, using flow model divided into near wake and adjacent regions
Hall, C. R., Jr.↗
On the energy transport in stellar winds
Stellar wind flow models associating energy transport with propagation and dissipation of hydrodynamic waves and heat conduction
Barnes, A.↗
Recompression of a two-dimensional supersonic turbulent free shear layer
Two dimensional supersonic turbulent free shear layer recompression process from flow model numerical calculation
Chow, W. L.↗
The theoretical and experimental investigations on multiple pure tone noise, part 1
A theoretical and experimental investigation is described on multiple pure tone noise. Based on a two-dimensional and inviscid flow model, an analysis is developed to predict the generation and subsequent evolution of multiple pure tone noise from prescribed blade-to-blade nonuniformities in the rotor geometry. The results show that even small nonuniformities within manufacturing tolerances can cause a significant amount of multiple pure tone noise. Among the different kinds of nonuniformities investigated, errors in blade spacings are a weaker generator of multiple pure tone noise than errors in blade stagger or blade contours. Experimental investigations of the effects of the rotor relative Mach number, incidence angle and length of the inlet duct on the evolution of the multiple pure tone noise are conducted with a known distribution of rotor nonuniformities. The model fan is operated, in Freon 12, in a closed loop acoustical facility.
Kantola, R. A.↗