AERODYNAMIC DESIGN OF THREE-DIMENSIONAL SUBSONIC WIND TUNNEL INLETS.

被引：0

作者：

Batill, Stephen M. ^{[1
]}

Hoffman, Joseph J. ^{[1
]}

机构：

[1] Univ of Notre Dame, Dep of Aerospace, & Mechanical Engineering, Notre, Dame, IN, USA, Univ of Notre Dame, Dep of Aerospace & Mechanical Engineering, Notre Dame, IN, USA

来源：

| 1600年 / 24期

关键词：

AERODYNAMICS - Inlets - FLOW OF FLUIDS - Potential Flow;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

A numerical study was conducted in order to establish a set of preliminary design guidelines and performance criteria for three-dimensional subsonic wind tunnel contraction sections. Inlet geometries for both square and rectangular cross-sectional inlets were considered for a range of contraction ratios of 10-40. Wall geometries were defined using a single-parameter, matched cubic profile. Finite difference field solutions were developed for a potential flow model and the inlet performance quantitied in terms of mean flowfield distortion and adverse wall pressure gradients. A turbulent boundary-layer separation prediction is included based on Stratford's criteria.

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