Aerodynamic Optimization Using Sensitivity Derivatives from a Three-Dimensional Supersonic Euler Code

Initial results from a three-dimensional marching Euler code equipped with an efficient sensitivity analysis capability are presented. The aerodynamic sensitivity derivatives with respect to wing geometry parameters obtained by the incremental iterative method are compared with those obtained by an...

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Veröffentlicht in:	Journal of aircraft 1998-05, Vol.35 (3), p.405-411
Hauptverfasser:	Korivi, Vamshi Mohan, Newman, Perry A, Taylor, Arthur C
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Aircraft Applied sciences Exact sciences and technology Fluid dynamics Geometry Ground, air and sea transportation, marine construction Miscellaneous transportation
Online-Zugang:	Volltext
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