Simulation of flow about rotating forebodies at high angles of attack

被引：0
|
作者：
机构：
[1] [1,Saephan, S.
[2] 1,Van Dam, C.P.
[3] 2,Fremaux, C.M.
[4] 3,DalBello, T.
来源：
Saephan, S. (ssaephan@ucdavis.edu) | 1600年 / American Institute of Aeronautics and Astronautics Inc.卷 / 41期
关键词：
Computer simulation - Control systems - Mathematical models - Navier Stokes equations - Reynolds number - Stability - Wind tunnels;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
A Reynolds-averaged Navier-Stokes flow solver is used to predict the forces and moments on forebody models at high angle-of-attack rotary conditions. Cases simulated using either a circular or square ogive at an angle of attack of 60 deg, freestream Mach number of 0.21, and Reynolds number based on body diameter of approximately two million are presented and compared against wind-tunnel data from rotary testing on generic forebody models conducted by NASA Langley Research Center and the Defence Research Agency in the United Kingdom. The simulations provide insight into the flow characteristics at steady rotary conditions.
引用
收藏
相关论文
共 50 条
  • [21] SUBSONIC-FLOW INVESTIGATION ON A RESEARCH BODY AT HIGH ANGLES OF ATTACK
    CLARKSON, MH
    MALCOLM, GN
    CHAPMAN, GT
    ASTRONAUTICS & AERONAUTICS, 1977, 15 (10): : B9 - B9
  • [22] A Study of Model Separation Flow Behavior at High Angles of Attack Aerodynamics
    Roy, A.
    Mallik, A. K.
    Sarma, T. P.
    JOURNAL OF APPLIED AND COMPUTATIONAL MECHANICS, 2018, 4 (04): : 318 - 330
  • [23] Plasma control of vortex flow on a delta wing at high angles of attack
    Sidorenko, Andrey A.
    Budovskiy, Alexey D.
    Maslov, Anatoly A.
    Postnikov, Boris V.
    Zanin, Boris Yu.
    Zverkov, Ilya D.
    Kozlov, Victor V.
    EXPERIMENTS IN FLUIDS, 2013, 54 (08)
  • [24] Flow control over a maneuvering delta wing at high angles of attack
    Klute, SM
    Rediniotis, OK
    Telionis, DP
    AIAA JOURNAL, 1996, 34 (04) : 662 - 668
  • [25] Investigation of asymmetric flow past a slender body at high angles of attack
    Osama Obeid
    Ibraheem AlQadi
    Jaber AlMutairi
    Theoretical and Computational Fluid Dynamics, 2019, 33 : 481 - 508
  • [26] Three-dimensional supersonic turbulent flow about bodies at small angles of attack
    Utyuzhnikov, SV
    Yamaleev, NK
    HIGH TEMPERATURE, 1996, 34 (04) : 562 - 567
  • [27] Sideslip behavior of elliptic cross-sectional forebodies at high angle of attack
    Tajfar, AH
    Lamont, PJ
    JOURNAL OF AIRCRAFT, 1997, 34 (04): : 472 - 478
  • [28] Flow Control of a Slender Blunt-Nose Body at High Angles of Attack
    Sirangu, Vijaya
    Ng, T. Terry
    JOURNAL OF AIRCRAFT, 2012, 49 (06): : 1904 - 1912
  • [29] VORTICAL FLOW OVER AN ELLIPTICAL-BODY MISSILE AT HIGH ANGLES OF ATTACK
    NEWSOME, RW
    ADAMS, MS
    JOURNAL OF SPACECRAFT AND ROCKETS, 1988, 25 (01) : 24 - 30
  • [30] Unsteady airloads on static airfoils through high angles of attack and in reverse flow
    Lind, Andrew H.
    Jones, Anya R.
    JOURNAL OF FLUIDS AND STRUCTURES, 2016, 63 : 259 - 279
12345