Criterion for Spanwise Spacing of Stall Cells-Reference-Cited by-同舟云学术

Criterion for Spanwise Spacing of Stall Cells

Published:2015-01 Issue:1 Volume:53 Page:272-274
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Gross Andreas¹,Fasel Hermann F.²,Gaster Michael³

Affiliation:

1. Mechanical and Aerospace Engineering Department, New Mexico State University, Las Cruces, New Mexico 88003

2. Aerospace and Mechanical Engineering Department, University of Arizona, Tucson, Arizona 85721

3. School of Engineering and Materials Science, University of London, London, England E1 4NS, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053347

Reference10 articles.

1. GregoryN.QuniceyV. G.O’ReillyC. L.HallD. J. “Progress Report on Observations of Three-Dimensional Flow Patterns Obtained During Stall Development on Airfoils and on the Problems of Measuring Two-Dimensional Characteristics,” Aeronautical Research CouncilCP-1146, 1971.

2. Flowfield Model for a Rectangular Planform Wing beyond Stall

3. BippesH.JacobK.TurkM. “Experimental Investigation of the Separated Flow Around a Rectangular Wing,” DLR, German Aerospace Center Research Rept. 81-12, Göttingen, Germany, 1981.

4. Reynolds-number effects in flow around more-or-less bluff bodies

5. Study of the Unsteady Flow Features on a Stalled Wing

Cited by 19 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Three-dimensional separation over unswept cantilevered wings at a moderate Reynolds number;Physical Review Fluids;2023-01-19

2. Wake dynamics of tapered wings. Part II: an experimental study;AIAA SCITECH 2023 Forum;2023-01-19

3. Multidisciplinary Optimization for Weight Saving in a Variable Tapered Span-Morphing Wing Using Composite Materials—Application to the UAS-S4;Actuators;2022-04-27

4. Effects of a trailing-edge flap on stall cell characteristics of a NACA0012 wing;Flow;2022

5. Structural Sizing and Topology Optimization Based on Weight Minimization of a Variable Tapered Span-Morphing Wing for Aerodynamic Performance Improvements;Biomimetics;2021-09-26