TY - JOUR
T1 - Design optimization of hypersonic vehicles for boundary-layer stability
AU - Johnson, Heath B
AU - Alba, Christopher R.
AU - Bartkowicz, Matthew D.
AU - Drayna, Travis W.
AU - Candler, Graham V
PY - 2008/9/15
Y1 - 2008/9/15
N2 - In this work, we present a methodology for a shape-based hypersonic vehicle optimization driven by boundary-layer stability properties. Full Navier-Stokes CFD calculations are performed at each parametric design point for both axisymmetric and three-dimensional surface geometries. Boundary-layer stability analysis is then performed through application of the parabolized stability equations. The performance metric used for the optimization procedure is either the N factor, representing the integrated growth rate of naturallyoccurring disturbances in the boundary-layer, or a predicted boundary-layer transition location based on a correlation of the N factor with experimental results. Optimization then involves minimization or maximization of this value.
AB - In this work, we present a methodology for a shape-based hypersonic vehicle optimization driven by boundary-layer stability properties. Full Navier-Stokes CFD calculations are performed at each parametric design point for both axisymmetric and three-dimensional surface geometries. Boundary-layer stability analysis is then performed through application of the parabolized stability equations. The performance metric used for the optimization procedure is either the N factor, representing the integrated growth rate of naturallyoccurring disturbances in the boundary-layer, or a predicted boundary-layer transition location based on a correlation of the N factor with experimental results. Optimization then involves minimization or maximization of this value.
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U2 - 10.2514/6.2008-6221
DO - 10.2514/6.2008-6221
M3 - Conference article
AN - SCOPUS:85067318429
SN - 1048-5953
JO - Collection of Technical Papers - AIAA Applied Aerodynamics Conference
JF - Collection of Technical Papers - AIAA Applied Aerodynamics Conference
T2 - 26th AIAA Applied Aerodynamics Conference
Y2 - 18 August 2008 through 21 August 2008
ER -