2007 U.S. Air Force T&E Days 2007
DOI: 10.2514/6.2007-1615
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A Parametric Geometry Computational Fluid Dynamics (CFD) Study Utilizing Design of Experiments (DOE)

Abstract: Design of Experiments (DOE) techniques were applied to the Launch Abort System (LAS) of the NASA Crew Exploration Vehicle (CEV) parametric geometry Computational Fluid Dynamics (CFD) study to efficiently identify and rank the primary contributors to the integrated drag over the vehicles ascent trajectory. Typical approaches to these types of activities involve developing all possible combinations of geometries changing one variable at a time, analyzing them with CFD, and predicting the main effects on an aerod… Show more

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Cited by 7 publications
(6 citation statements)
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“…This method is similar to the analysis technique presented by Rhew and Parker [29]. Following the 2 Â 2 Â 2 factorial analysis, two 2-factor two-level analyses were conducted to consider the effects of geometry on untreated and treated aneurysm hemodynamics separately.…”
Section: Discussionmentioning
confidence: 99%
“…This method is similar to the analysis technique presented by Rhew and Parker [29]. Following the 2 Â 2 Â 2 factorial analysis, two 2-factor two-level analyses were conducted to consider the effects of geometry on untreated and treated aneurysm hemodynamics separately.…”
Section: Discussionmentioning
confidence: 99%
“…Contributions of the geometric factors (and their interactions) toward modifying hemodynamic responses were then calculated by dividing individual SS values by the total SS. More detail on related statistical analyses can be found in Rhew et al (Rhew and Parker, 2007). Hemodynamic responses were also compared directly between the ABTA models and their matching IBTA counterparts using Pearson correlation.…”
Section: Computational Data Analysismentioning
confidence: 99%
“…Despite the availability of high performance computing (HPC) facilities, the routine use of computational fluid dynamics (CFD) is yet restricted to a pre-defined (small) number of configurations. Two remarkable studies are those of Rogers et al (2003) at NASA Ames and of Rhew and Parker (2007) at NASA Langley. The reasons that linear methods have cornered the industrial aircraft design process are twofold.…”
Section: Introductionmentioning
confidence: 99%