UNSTEADY-FLOW PAST AN AIRFOIL WITH THICKNESS SUBJECT TO A 2-DIMENSIONAL GUST

被引:0
|
作者
HAMAD, G [1 ]
ATASSI, H [1 ]
机构
[1] UNIV NOTRE DAME,NOTRE DAME,IN 46556
来源
关键词
D O I
暂无
中图分类号
O4 [物理学];
学科分类号
0702 ;
摘要
引用
收藏
页码:1127 / 1127
页数:1
相关论文
共 50 条
  • [1] UNSTEADY-FLOW PAST AN AIRFOIL PITCHING AT A CONSTANT RATE
    SHIH, C
    LOURENCO, L
    VANDOMMELEN, L
    KROTHAPALLI, A
    [J]. AIAA JOURNAL, 1992, 30 (05) : 1153 - 1161
  • [2] COMPLETE 2ND-ORDER THEORY FOR UNSTEADY-FLOW ABOUT AN AIRFOIL DUE TO A PERIODIC GUST
    GOLDSTEIN, ME
    ATASSI, H
    [J]. JOURNAL OF FLUID MECHANICS, 1976, 74 (APR22) : 741 - 765
  • [3] ON THE FLOW AT THE REAR OF A 2-DIMENSIONAL SUPERSONIC AIRFOIL WITH THICKNESS
    PROBSTEIN, RF
    [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (08): : 580 - 581
  • [4] 2-DIMENSIONAL UNSTEADY-FLOW AROUND A WAVING PLATE IN WALL EFFECTS
    ZHUANG, LX
    SHIDA, Y
    TAKAMI, H
    [J]. FLUID DYNAMICS RESEARCH, 1990, 5 (5-6) : 321 - 336
  • [5] FINITE-VOLUME 2-DIMENSIONAL UNSTEADY-FLOW MODEL FOR RIVER BASINS
    ZHAO, DH
    SHEN, HW
    TABIOS, GQ
    LAI, JS
    TAN, WY
    [J]. JOURNAL OF HYDRAULIC ENGINEERING-ASCE, 1994, 120 (07): : 863 - 883
  • [6] UNSTEADY-FLOW PHENOMENA IN CENTRIFUGAL FANS .2. 3 DIMENSIONAL UNSTEADY-FLOW MEASUREMENT
    KUBO, T
    [J]. BULLETIN OF THE JSME-JAPAN SOCIETY OF MECHANICAL ENGINEERS, 1980, 23 (185): : 1771 - 1778
  • [7] NUMERICAL-SOLUTIONS OF 2-DIMENSIONAL MULTISTAGE ROTOR/STATOR UNSTEADY-FLOW INTERACTIONS
    YANG, RJ
    LIN, SJ
    [J]. JOURNAL OF PROPULSION AND POWER, 1994, 10 (06) : 876 - 883
  • [8] UNSTEADY-FLOW ABOUT A JOUKOWSKI AIRFOIL IN THE PRESENCE OF MOVING VORTICES
    CHOW, CY
    HUANG, MK
    YAN, CZ
    [J]. AIAA JOURNAL, 1985, 23 (05) : 657 - 658
  • [9] THE FLOW AT THE REAR OF A 2-DIMENSIONAL SUPERSONIC AIRFOIL
    KAHANE, A
    LEES, L
    [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1948, 15 (03): : 167 - 170
  • [10] METHOD FOR CALCULATING THE UNSTEADY-FLOW OF AN ELLIPTICAL CIRCULATION-CONTROL AIRFOIL
    MAO, S
    WEI, W
    [J]. JOURNAL OF AIRCRAFT, 1989, 26 (10): : 907 - 913