Flow structure generated by oscillating delta-wing segments

被引：0
|
作者：
机构：
[1] Utsch, Thomas
[2] Rockwell, Donald
来源：
Utsch, Thomas | 1600年 / 27期
关键词：
Aircraft;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
相关论文
共 50 条
  • [41] Direct measurement of delta-wing vortex circulation
    Johari, H
    Moreira, J
    AIAA JOURNAL, 1998, 36 (12) : 2195 - 2203
  • [42] DYNAMIC PITCH-UP OF A DELTA-WING
    REDINIOTIS, OK
    KLUTE, SM
    HOANG, NT
    TELIONIS, DP
    AIAA JOURNAL, 1994, 32 (04) : 716 - 725
  • [43] CONICAL EULER SIMULATION OF WING ROCK FOR A DELTA-WING PLANFORM
    LEE, EM
    BATINA, JT
    JOURNAL OF AIRCRAFT, 1991, 28 (01): : 94 - 96
  • [44] Rapid prediction of wing rock for slender delta-wing configurations
    Ericsson, LE
    JOURNAL OF AIRCRAFT, 1998, 35 (06): : 979 - 981
  • [45] FORCE MEASUREMENTS ON A REFLEX CAMBERED DELTA-WING
    HOLLA, VS
    ARAVAMUDHAN, MD
    RAO, PJ
    JOURNAL OF AIRCRAFT, 1982, 19 (06): : 417 - 418
  • [46] NUMERICAL STUDY OF HYPERSONIC LEEWARD FLOW OVER A BLUNT NOSED DELTA-WING
    MALLETT, ER
    PULLIN, DI
    MACROSSAN, MN
    AIAA JOURNAL, 1995, 33 (09) : 1626 - 1633
  • [47] NUMERICAL-ANALYSIS OF THE VORTICAL FLOW AROUND A DELTA-WING CANARD CONFIGURATION
    DAS, A
    LONGO, JMA
    JOURNAL OF AIRCRAFT, 1995, 32 (04): : 716 - 725
  • [48] INFLUENCE OF SIDESLIP ON DOUBLE DELTA-WING AERODYNAMICS
    GRISMER, DS
    NELSON, RC
    ELY, WL
    JOURNAL OF AIRCRAFT, 1995, 32 (02): : 451 - 453
  • [49] EFFECT OF A FUSELAGE ON DELTA-WING VORTEX BREAKDOWN
    STRAKA, WA
    HEMSCH, MJ
    JOURNAL OF AIRCRAFT, 1994, 31 (04): : 1002 - 1005
  • [50] EARLY VORTEX BURST ON A DELTA-WING IN PITCH
    SOLTANI, MR
    BRAGG, MB
    AIAA JOURNAL, 1993, 31 (12) : 2283 - 2289
12345