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WINGS CONTOURED INCONTINENT BRIEF XX-LARGE

Known as: WINGS CONTOURED INCONTINENT BRIEF XX-LG 
National Institutes of Health

Papers overview

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2014
2014
Contoured nozzle used for shock tunnel was designed and validated. Inviscid nozzle contour was attained through MOC and boundary… 
2011
2011
Secondary flow minimization is a crucial problem in a turbine passage. In the present paper, three different ways are employed to… 
2009
2009
The detection of actual changes in a pair of images is confounded by the inadvertent but pervasive differences that inevitably… 
Review
2006
Review
2006
This dissertation develops a novel computationally feasible intelligent data mining and knowledge discovery technique to select… 
2004
2004
Turbine manufacturers continually seek to gain efficiency by increasing operating temperatures well above the maximum temperature… 
1999
1999
For many years, GE has been conducting research to better understand the loss mechanisms that degrade the aerodynamic performance…