Inviscid separated flow over a non-slender delta wing

被引：0
作者：
Moore, D.W. [1 ]
Pullin, D.I. [1 ]
机构：
[1] Imperial Coll of Science, Technology and Medicine, London, United Kingdom
来源：
Journal of Fluid Mechanics | 1995年 / 305卷
关键词：
15;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：307 / 345
相关论文
共 50 条
[11]   Effect of ground on aerodynamics and longitudinal static stability of a non-slender delta wing [J].
Kocak, Goktug ;
Yavuz, Mehmet Metin .
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 130
[12]   Effect of thickness-to-chord ratio on aerodynamics of non-slender delta wing [J].
Ghazijahani, Mohammad Sharifi ;
Yavuz, Mehmet Metin .
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 88 :298-307
[13]   Experimental investigation of dynamic ground boundary condition for a non-slender delta wing [J].
Koçak G. ;
Yavuz M.M. .
CEAS Aeronautical Journal, 2024, 15 (04) :957-976
[14]   SEPARATED FLOW PAST A SLENDER DELTA WING AT INCIDENCE. [J].
Barsby, J.E. .
1973, 24 (Pt 2) :120-128
[15]   Characterization of the Flow Field of Slender and Non-Slender Delta Wings using Volumetric PIV [J].
Smith, Antoine ;
Balogun, Hakeem ;
Khan, M. Javed ;
Aji, Chadia A. ;
Salehian, Saman .
AIAA SCITECH 2022 FORUM, 2022,
[16]   Aerodynamics of non-slender delta and reverse delta wings: Wing thickness, anhedral angle and cropping ratio [J].
Gktu KOAK ;
Mehmet Metin YAVUZ .
Chinese Journal of Aeronautics , 2023, (04) :79-91
[17]   Aerodynamics of non-slender delta and reverse delta wings: Wing thickness, anhedral angle and cropping ratio [J].
Kocak, Goktug ;
Yavuz, Mehmet Metin .
CHINESE JOURNAL OF AERONAUTICS, 2023, 36 (04) :79-91
[18]   Low speed aerodynamic characteristics of non-slender delta wing at low angles of attack [J].
Mohamed, Mohamed A. ;
Afgan, Imran ;
Salim, Mohamed Hefny ;
Mohamed, Ibrahim K. .
ALEXANDRIA ENGINEERING JOURNAL, 2022, 61 (12) :9427-9435
[19]   Aerodynamics of non-slender delta and reverse delta wings: Wing thickness, anhedral angle and cropping ratio [J].
Gktu KOAK ;
Mehmet Metin YAVUZ .
Chinese Journal of Aeronautics, 2023, 36 (04) :79-91
[20]   Further analysis of self-induced roll oscillations of a non-slender delta wing [J].
Beyers, M. E. ;
Ericsson, L. E. .
AERONAUTICAL JOURNAL, 2006, 110 (1113) :739-748
12345