郑州大学学报（理学版）2019，Vol.51Issue(1)：95-100,6.DOI:10.13705/j.issn.1671-6841.2018080
跨音速自然层流翼型反设计研究
Inverse Design of the Transonic Natural Laminar Flow Airfoil
摘要
Abstract
The inverse design method was studied based on gappy proper orthogonal decomposition ( POD) . According to surface pressure distribution, the gappy POD reduced order model was used to re-construct missing data of an airfoil. In the initial snapshot sampling process, ΔCST was used to get the snapshot, then the basic airfoil was replaced by the inverse designed, and the new snapshot designed by POD was added to snapshot. For laminar flow airfoil inverse design, pressure distribution snapshot were got by γ-Reθtransition model. Two different pressure distributions of the transonic NLF airfoil were pro-posed. Then two transonic NLF airfoils could be obtained by the inverse design method. The ability for postponing the transition of different pressure distributions under different Reynolds number and Mach numbers were studied in detail.关键词
CST/自然层流翼型/转捩模型/反设计Key words
CST/NLF airfoil/transition model/inverse design分类
航空航天引用本文复制引用
李静,刘艳萍,高正红,梁天水..跨音速自然层流翼型反设计研究[J].郑州大学学报（理学版）,2019,51(1):95-100,6.基金项目
国家自然科学基金项目(11602226) （11602226）
河南省高等学校重点科研项目(16A130001). （16A130001）
