EXPERIMENTAL PRESSURE EVALUATION NEAR A SAIL LEADING-EDGE UNDER REAL CONDITIONS

被引:0
|
作者
LOMBARDI, G
TONELLI, A
机构
[1] Univ of Pisa, Italy
来源
AERONAUTICAL JOURNAL | 1994年 / 98卷 / 978期
关键词
Aerodynamics;
D O I
10.1017/S0001924000026828
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The aerodynamic condition corresponding to the optimum sail trim has been long debated; in the present note this aerodynamic aspect of the sails is studied by means of pressure measurements near the sail leading-edge. By analysing the pressure acting on the leading edge zone it can be evidenced that, when the sail is ''optimally'' trimmed, it is actually in the aerodynamic condition corresponding to the ideal angle of attack.
引用
收藏
页码:319 / 322
页数:4
相关论文
共 50 条
  • [41] Experimental investigation of the sound reduction by leading-edge serrations in axial fans
    1600, AIAA International, 12700 Sunrise Valley Drive, Suite 200Reston, VA, Virginia, Virginia 20191-5807, United States (56):
  • [42] Experimental investigation of ground effects on aerodynamics of sinusoidal leading-edge wings
    Mehraban, A. A.
    Djavareshkian, M. H.
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART C-JOURNAL OF MECHANICAL ENGINEERING SCIENCE, 2021, 235 (19) : 3988 - 4001
  • [43] An experimental study on turbine vane Leading-Edge film cooling with deposition
    Yang, Xing
    Hao, Zihan
    Feng, Zhenping
    APPLIED THERMAL ENGINEERING, 2021, 198
  • [44] Turbulence Modeling for Leading-Edge Vortices: An Enhancement Based on Experimental Data
    Moioli, Matteo
    Breitsamter, Christian
    Sorensen, Kaare A.
    AIAA JOURNAL, 2022, 60 (03) : 1382 - 1399
  • [45] Thermohydrodynamic modeling of leading-edge groove bearings under starvation condition
    He, M
    Allaire, P
    Barrett, L
    Nicholas, J
    TRIBOLOGY TRANSACTIONS, 2005, 48 (03) : 362 - 369
  • [46] A simplified model for drag evaluation of a streamlined body with leading-edge damage
    Yu, Haoliang
    Ciri, Umberto
    Malik, Arif
    Leonardi, Stefano
    JOURNAL OF TURBULENCE, 2021, 22 (10): : 656 - 679
  • [47] EVALUATION OF NAVIER STOKES AND EULER SOLUTIONS FOR LEADING-EDGE SEPARATION VORTICES
    FUJII, K
    GAVALI, S
    HOLST, TL
    INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS, 1988, 8 (10) : 1319 - 1329
  • [48] Characteristics of a separated flow past a semicircular leading-edge airfoil model under different imposed pressure gradient
    Anand, K.
    Ganesh, K. T.
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2022, 236 (04) : 722 - 738
  • [49] PRESSURE-GRADIENT AND LEADING-EDGE EFFECTS ON THE CORNER BOUNDARY-LAYER
    ZAMIR, M
    YOUNG, AD
    AERONAUTICAL QUARTERLY, 1979, 30 (AUG): : 471 - 484
  • [50] Features of a Laminar Separated Boundary Layer Near the Leading-Edge of a Model Airfoil for Different Angles of Attack: An Experimental Study
    Anand, K.
    Sarkar, S.
    JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 2017, 139 (02):