Two-dimensional unsteady leading-edge separation on a pitching airfoil

被引：0

作者：

Choudhuri, P.Ghosh ^{[1
]}

Knight, D.D. ^{[1
]}

Visbal, M.R. ^{[1
]}

机构：

[1] Rutgers Univ, Piscataway, United States

来源：

| 1600年 / 32期

关键词：

Subsonic aerodynamics;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

引用

共 50 条

[1] 2-DIMENSIONAL UNSTEADY LEADING-EDGE SEPARATION ON A PITCHING AIRFOIL
CHOUDHURI, PG
KNIGHT, DD
VISBAL, MR
AIAA JOURNAL, 1994, 32 (04) : 673 - 681
[2] NUMERICAL STUDY OF UNSTEADY LEADING-EDGE SEPARATION BUBBLE ON AN OSCILLATING AIRFOIL
KRESKOVSKY, JP
SHAMROTH, SJ
BRILEY, WR
COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 1977, 11 (01) : 39 - 56
[3] Aerodynamic characteristics of a pitching airfoil with leading-edge morphing
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ChineseJournalofAeronautics, 2024, 37 (07) : 81 - 92
[4] Aerodynamic characteristics of a pitching airfoil with leading-edge morphing
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[5] Controlled leading-edge suction for management of unsteady separation over pitching airfoils
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[6] Effects of compressibility, pitch rate, and Reynolds number on unsteady incipient leading-edge boundary layer separation over a pitching airfoil
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[7] Numerical investigation on effect of leading-edge deformation to alleviate dynamic stall of pitching airfoil in unsteady flow
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WIND ENGINEERING, 2024, 48 (06) : 1157 - 1173
[8] Leading-Edge Flow Structure of a Dynamically Pitching NACA 0012 Airfoil
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AIAA JOURNAL, 2013, 51 (05) : 1042 - 1053
[9] Leading-edge flow structure of a dynamically pitching NACA 0012 airfoil
1600, AIAA International (51):
[10] Leading-edge flow criticality as a governing factor in leading-edge vortex initiation in unsteady airfoil flows
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Theoretical and Computational Fluid Dynamics, 2018, 32 : 109 - 136

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