Numerical investigation of crossflow separation on a tangent-ogive forebody at high angle of attack

被引：2

作者：

Onn, SC ^{[1
]}

Yang, NC ^{[1
]}

Hsiung, JL ^{[1
]}

Wei, CK ^{[1
]}

机构：

[1] CHUNG SHAN INST SCI & TECHNOL, TAYUAN, TAIWAN

来源：

JSME INTERNATIONAL JOURNAL SERIES B-FLUIDS AND THERMAL ENGINEERING | 1997年 / 40卷 / 01期

关键词：

crossflow separation; high angle of attack; turbulence model; subsonic flow; sublayer-mass flow method;

D O I：

10.1299/jsmeb.40.75

中图分类号：

O414.1 [热力学];

学科分类号：

摘要：

A ''sublayer-mass flow'' method is developed as a new tool for analysis of crossflow separation. It is found that the critical points of sublayer-mass flow are located at the points of convergence of surface streamlines. Thus, the critical points indicate where the flow is separated. This representation can be used to identify the primary and secondary separation points of crossflow separation. This is the first successful capture of crossflow separation points in a three-dimensional flow computation.

引用

页码：75 / 80

页数：6

共 50 条

[41] NUMERICAL INVESTIGATION ON THE COANDA EFFECT OVER THE S809 AIRFOIL WITH SYNTHETIC JET ACTUATOR AT HIGH ANGLE OF ATTACK
Moshfeghi, Mohammad
Nur, Nahmkeon
PROCEEDINGS OF THE ASME FLUIDS ENGINEERING DIVISION SUMMER MEETING - 2014, VOL 1B: SYMPOSIA, 2014,
[42] Numerical Investigation on Evolution of Tip Vortices Generated by Low-Aspect Ratio Rectangular Wings at High Angle of Attack
Lee, Jae Hoon
Han, Yong Oun
INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2019, 20 (01) : 44 - 56
[43] Numerical Investigation on Evolution of Tip Vortices Generated by Low-Aspect Ratio Rectangular Wings at High Angle of Attack
Jae Hoon Lee
Yong Oun Han
International Journal of Aeronautical and Space Sciences, 2019, 20 : 44 - 56
[44] INVESTIGATION ON STABILITY IN ROLL OF SQUARE SECTION MISSILE AT HIGH ANGLE OF ATTACK
Tao, Yang
Fan, Zhaolin
Wu, Jifei
Wu, Wenhua
MODERN PHYSICS LETTERS B, 2010, 24 (13): : 1385 - 1388
[45] Numerical investigation of the origin of vortex asymmetry of flows over bodies at large angle of attack
Degani, D.
Congress of the International Council of the Aeronautical Sciences - ICAS Proceedings, 1990,
[46] Numerical analysis on the vortex motion and bursting of delta wing at high angle of attack
Zhang, Li
Wang, Liangyi
Nanjing Hangkong Hangtian Daxue Xuebao/Journal of Nanjing University of Aeronautics and Astronautics, 1994, 26 (04): : 442 - 448
[47] Vortex formation and shedding from an airfoil at high angle of attack: a numerical study
Breuer, M
Jovicic, N
COMPUTATIONAL FLUID AND SOLID MECHANICS 2003, VOLS 1 AND 2, PROCEEDINGS, 2003, : 858 - 861
[48] Numerical Studies of Aerodynamic Performance of Gapped Flat Plates at High Angle of Attack
Tian, De
He, Wei
Wang, Weilong
MATERIALS, MECHANICAL ENGINEERING AND MANUFACTURE, PTS 1-3, 2013, 268-270 : 1172 - 1176
[49] Numerical investigation of plasma actuator configurations for flow separation control at multiple angles of attack
West IV, T.K. (tkwgg3@mst.edu), 1600, Multi-Science Publishing Co. Ltd, 5 Wates Way, Brentwood, Essex, CM15 9TB, United Kingdom (05):
[50] HIGH-ANGLE-OF-ATTACK WIND-TUNNEL INVESTIGATION OF A MULTIMISSION VEHICLE
HEBBAR, SK
PLATZER, MF
SMITH, EH
SALAZAR, ME
JOURNAL OF SPACECRAFT AND ROCKETS, 1995, 32 (04) : 734 - 736

← 1 2 3 4 5 →