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NASA Scientific and Technical Aerospace Reports

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experimental dataset provides essential flow-field information for the validation of near-field inputs to noise prediction tools.<br />

Author<br />

Unsteady Flow; Particle Image Velocimetry; Leading Edge Slats; Wind Tunnel Models; Aerodynamics; Characterization<br />

20040073477 QSS Group, Inc., Clevel<strong>and</strong>, OH, USA<br />

TopMaker: A Technique for Automatic Multi-Block Topology Generation Using the Medial Axis<br />

Heidmann, James D., <strong>Technical</strong> Monitor; Rigby, David L.; April 2004; 16 pp.; In English; Fourth Joint Fluids Engineering<br />

Conference, 6-10 Jul. 2003, Honolulu, HI, USA<br />

Contract(s)/Grant(s): NAS3-00145; WBS 22-714-09-11<br />

Report No.(s): <strong>NASA</strong>/CR-2004-213044; FEDSM2003-45527; E-14481; No Copyright; Avail: CASI; A03, Hardcopy<br />

A two-dimensional multi-block topology generation technique has been developed. Very general configurations are<br />

addressable by the technique. A configuration is defined by a collection of non-intersecting closed curves, which will be<br />

referred to as loops. More than a single loop implies that holes exist in the domain, which poses no problem. This technique<br />

requires only the medial vertices <strong>and</strong> the touch points that define each vertex. From the information about the medial vertices,<br />

the connectivity between medial vertices is generated. The physical shape of the medial edge is not required. By applying a<br />

few simple rules to each medial edge, the multiblock topology is generated with no user intervention required. The resulting<br />

topologies contain only the level of complexity dictated by the configurations. Grid lines remain attached to the boundary<br />

except at sharp concave turns where a change in index family is introduced as would be desired. Keeping grid lines attached<br />

to the boundary is especially important in the area of computational fluid dynamics where highly clustered grids are used near<br />

no-slip boundaries. This technique is simple <strong>and</strong> robust <strong>and</strong> can easily be incorporated into the overall grid generation process.<br />

Author<br />

Grid Generation (Mathematics); Multiblock Grids; Topology; Computational Fluid Dynamics; Two Dimensional Models<br />

20040073486 <strong>NASA</strong> Glenn Research Center, Clevel<strong>and</strong>, OH, USA<br />

Predictions for the Effects of Free Stream Turbulence on Turbine Blade Heat Transfer<br />

Boyle, Robert J.; Giel, Paul W.; Ames, Forrest E.; May 2004; 23 pp.; In English; Turbo Expo 2004, 14-17 Jun. 2004, Vienna,<br />

Austria<br />

Contract(s)/Grant(s): WBS 22-714-30-10<br />

Report No.(s): <strong>NASA</strong>/TM-2004-213079; GT2004-54332; E-14555; No Copyright; Avail: CASI; A03, Hardcopy<br />

An approach to predicting the effects of free stream turbulence on turbine vane <strong>and</strong> blade heat transfer is described. Four<br />

models for predicting the effects of free stream turbulence were in incorporated into a Navier-Stokes CFD analysis. Predictions<br />

were compared with experimental data in order to identify an appropriate model for use across a wide range of flow conditions.<br />

The analyses were compared with data from five vane geometries <strong>and</strong> from four rotor geometries. Each of these nine<br />

geometries had data for different Reynolds numbers. Comparisons were made for twenty four cases. Steady state calculations<br />

were done because all experimental data were obtained in steady state tests. High turbulence levels often result in suction<br />

surface transition upstream of the throat, while at low to moderate Reynolds numbers the pressure surface remains laminar.<br />

A two-dimensional analysis was used because the flow is predominately two-dimensional in the regions where free stream<br />

turbulence significantly augments surface heat transfer. Because the evaluation of models for predicting turbulence effects can<br />

be affected by other factors, the paper discusses modeling for transition, relaminarization, <strong>and</strong> near wall damping. Quantitative<br />

comparisons are given between the predictions <strong>and</strong> data.<br />

Author<br />

Computational Fluid Dynamics; Heat Transfer; Turbine Blades; Free Flow; Mathematical Models; Turbulence; Rotor<br />

Dynamics<br />

20040073495 <strong>NASA</strong> Marshall Space Flight Center, Huntsville, AL, USA<br />

An Overview of the Materials Science Research at the Marshall Space Flight Center Electrostatic Levitator Facility<br />

<strong>and</strong> Recent CDDF Efforts<br />

Biological <strong>and</strong> Physical Space Research Laboratory 2002 Science Review; December 2003, pp. 17; In English; See also<br />

20040073490; No Copyright; Abstract Only; Available from CASI only as part of the entire parent document<br />

Containerless processing is an important tool for materials research. The freedom from a crucible allows processing of<br />

liquid materials in a metastable undercooled state, as well as allowing processing of high temperature <strong>and</strong> highly reactive<br />

melts. Electrostatic levitation (ESL) is a containerless method which provides a number of unique advantages, including the<br />

ability to process non-conducting materials, the ability to operate in ultra-high vacuum or at moderate gas pressure (approx.<br />

93

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