Transonic rotor blade pressure measurement using fluorescent paints

被引：3
|
作者：
Liu, T [1 ]
Torgerson, S
Sullivan, J
Johnston, R
Fleeter, S
机构：
[1] NASA, Langley Res Ctr, Hampton, VA 23681 USA
[2] LM Aero, Palmdale, CA 93550 USA
[3] Purdue Univ, Sch Aeronaut & Astronaut, W Lafayette, IN 47907 USA
[4] Pratt & Whitney, Middletown, CT 06457 USA
[5] Purdue Univ, Sch Mech Engn, W Lafayette, IN 47907 USA
来源：
JOURNAL OF PROPULSION AND POWER | 2002年 / 18卷 / 02期
关键词：
D O I：
10.2514/2.5961
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：491 / 493
页数：3
相关论文
共 50 条
  • [31] Comparison of Flow Mechanism of Blade Sweep between a Transonic Single Rotor and a Rotor in Stage Environment
    Cao, Zhiyuan
    Gao, Xi
    Liang, Yuyuan
    Huang, Ping
    Lei, Peng
    Liu, Bo
    JOURNAL OF THERMAL SCIENCE, 2022, 31 (05) : 1804 - 1819
  • [32] Optimization Of Rotor Blade In Stage Circumstance For Transonic Axial Flow Compressor
    Cheng, Jinxin
    Chen, Jiang
    Xiang, Hang
    PROCEEDINGS OF THE 2017 12TH IEEE CONFERENCE ON INDUSTRIAL ELECTRONICS AND APPLICATIONS (ICIEA), 2017, : 1774 - 1779
  • [33] Aeroelastic prediction and analysis for a transonic fan rotor with the "hot" blade shape
    Zhou, Di
    Lu, Ziliang
    Guo, Tongqing
    Chen, Guoping
    CHINESE JOURNAL OF AERONAUTICS, 2021, 34 (07) : 50 - 61
  • [34] Measurement of helicopter rotor blade deformation using digital image correlation
    Sirohi, Jayant
    Lawson, Michael S.
    OPTICAL ENGINEERING, 2012, 51 (04)
  • [35] MEASUREMENT AROUND A ROTOR BLADE EXCITED IN PITCH .2. UNSTEADY SURFACE PRESSURE
    LAL, MK
    LIOU, SG
    PIERCE, GA
    KOMERATH, NM
    JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 1994, 39 (02) : 13 - 20
  • [36] Effect of blade tip winglet on the performance of a highly loaded transonic compressor rotor
    Han Shaobing
    Zhong Jingjun
    CHINESE JOURNAL OF AERONAUTICS, 2016, 29 (03) : 653 - 661
  • [37] Effect of blade tip winglet on the performance of a highly loaded transonic compressor rotor
    Han Shaobing
    Zhong Jingjun
    Chinese Journal of Aeronautics, 2016, 29 (03) : 653 - 661
  • [38] Experimental investigation of the perpendicular rotor blade-vortex interaction at transonic speeds
    Kalkhoran, Iraj M., 1600, (30):
  • [39] Statistical evaluation of performance impact of flow variations for a transonic compressor rotor blade
    Xia, Zhiheng
    Luo, Jiaqi
    Liu, Feng
    ENERGY, 2019, 189
  • [40] Effect of blade tip winglet on the performance of a highly loaded transonic compressor rotor
    Han Shaobing
    Zhong Jingjun
    Chinese Journal of Aeronautics , 2016, (03) : 653 - 661
12345