| タイトル | Three-dimensional aerodynamic shape optimization of supersonic delta wings |
| 本文（外部サイト） | http://hdl.handle.net/2060/19960008979 |
| 著者（英） | Baysal, Oktay; Burgreen, Greg W. |
| 著者所属（英） | Old Dominion Univ. |
| 発行日 | 1994-09-09 |
| 言語 | eng |
| 内容記述 | A recently developed three-dimensional aerodynamic shape optimization procedure AeSOP(sub 3D) is described. This procedure incorporates some of the most promising concepts from the area of computational aerodynamic analysis and design, specifically, discrete sensitivity analysis, a fully implicit 3D Computational Fluid Dynamics (CFD) methodology, and 3D Bezier-Bernstein surface parameterizations. The new procedure is demonstrated in the preliminary design of supersonic delta wings. Starting from a symmetric clipped delta wing geometry, a Mach 1.62 asymmetric delta wing and two Mach 1. 5 cranked delta wings were designed subject to various aerodynamic and geometric constraints. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 96N16145
NASA-CR-199744
NAS 1.26:199744
AIAA PAPER 94-4271
NIPS-95-06437 |
| 権利 | Copyright, Distribution under U.S. Government purpose rights |
