ADAPTIVE-WALL WIND-TUNNEL DEVELOPMENT FOR TRANSONIC TESTING

被引:3
|
作者
SATYANARAYANA, B
SCHAIRER, E
DAVIS, S
机构
来源
JOURNAL OF AIRCRAFT | 1981年 / 18卷 / 04期
关键词
D O I
10.2514/3.44701
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:273 / 279
页数:7
相关论文
共 50 条
  • [1] CONVERGENCE OF ADAPTIVE-WALL WIND-TUNNEL
    LO, CF
    KRAFT, EM
    [J]. AIAA JOURNAL, 1978, 16 (01) : 67 - 72
  • [2] CONVERGENCE SCHEMES FOR AN ADAPTIVE-WALL WIND-TUNNEL
    CELIK, ZZ
    BODAPATI, S
    [J]. JOURNAL OF AIRCRAFT, 1988, 25 (08): : 733 - 739
  • [3] INTERFERENCE-FREE WIND-TUNNEL FLOWS BY ADAPTIVE-WALL TECHNOLOGY
    SEARS, WR
    VIDAL, RJ
    ERICKSON, JC
    RITTER, A
    [J]. JOURNAL OF AIRCRAFT, 1977, 14 (11): : 1042 - 1050
  • [4] NUMERICAL SIMULATIONS OF A SEGMENTED-PLENUM, PERFORATED, ADAPTIVE-WALL WIND-TUNNEL
    ERICKSON, JC
    HOMICZ, GF
    [J]. AIAA JOURNAL, 1982, 20 (05) : 612 - 623
  • [5] UNSTEADY ADAPTIVE WALL MODELS FOR WIND-TUNNEL TESTING
    CHANG, BH
    SUNG, BZ
    CHANG, KS
    [J]. AIAA JOURNAL, 1995, 33 (08) : 1536 - 1538
  • [6] TRANSONIC WIND-TUNNEL WALL INTERFERENCE MINIMIZATION
    GRUNNET, JL
    [J]. JOURNAL OF AIRCRAFT, 1984, 21 (09): : 694 - 699
  • [7] WIND-TUNNEL MODEL POSITION FOR TRANSONIC TESTING
    POPE, A
    [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1954, 21 (04): : 280 - 281
  • [8] 2-DIMENSIONAL ADAPTIVE-WALL TESTS IN THE NASA AMES 2-FOOT BY 2-FOOT TRANSONIC WIND-TUNNEL
    SCHAIRER, ET
    LEE, G
    MCDEVITT, TK
    [J]. JOURNAL OF AIRCRAFT, 1991, 28 (11): : 673 - 682
  • [9] DISTURBANCE OF TRANSONIC WIND-TUNNEL FLOW BY A SLOT IN THE TUNNEL WALL
    RISTIC, S
    [J]. EXPERIMENTS IN FLUIDS, 1991, 11 (06) : 403 - 404
  • [10] TRANSONIC WIND-TUNNEL WALL INTERFERENCE PREDICTION CODE
    PHILLIPS, PS
    WAGGONER, EG
    [J]. JOURNAL OF AIRCRAFT, 1990, 27 (11): : 915 - 916