Application of pressure sensitive paint on aerodynamic load measurement of delta wing model in supersonic wind tunnel

被引：0
|
作者：
Xiang, Xing-Ju [1 ]
Lang, Wei-Dong [1 ]
Xiong, Hong-Liang [1 ]
机构：
[1] China Academy of Aerospace Aerodynamics, Beijing 100074, China
来源：
Shiyan Liuti Lixue/Journal of Experiments in Fluid Mechanics | 2010年 / 24卷 / 03期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
11
引用
收藏
页码：81 / 86
相关论文
共 50 条
  • [21] Photogrammetry for accurate model deformation measurement in a supersonic wind tunnel
    Gramola, Michela
    Bruce, Paul J. K.
    Santer, Matthew
    EXPERIMENTS IN FLUIDS, 2019, 60 (01)
  • [22] Photogrammetry for accurate model deformation measurement in a supersonic wind tunnel
    Michela Gramola
    Paul J. K. Bruce
    Matthew Santer
    Experiments in Fluids, 2019, 60
  • [23] Light emitting surfaces of wind tunnel models for excitation of pressure sensitive paint
    Schulze, B
    Klein, C
    ICIASF '05 RECORD: 21ST INTERNATIONAL CONGRESS ON INSTRUMENTATION IN AEROSPACE SIMULATION FACILITIES, 2005, : 274 - 282
  • [24] Temperature correction of pressure-sensitive paint for industrial wind tunnel testing
    Kurita, Mitsuru
    Nakakita, Kazuyuki
    Mitsuo, Kazunori
    Watanabe, Shigeya
    JOURNAL OF AIRCRAFT, 2006, 43 (05): : 1499 - 1505
  • [25] First pressure-sensitive paint application at ONERA transonic wind tunnel S3Ch
    Mebarki, Y
    Merienne, MC
    INTERNATIONAL SEMINAR ON OPTICAL METHODS AND DATA PROCESSING IN HEAT AND FLUID FLOW, 1996, 1996 (03): : 507 - 516
  • [26] Application of Pressure Sensitive Paint for determination of aerodynamic loads and moments on propeller blade
    Kulesh, V. P.
    Mosharov, V. E.
    Orlov, A. A.
    Ostroukhov, S. P.
    Radchenko, V. N.
    OPTICAL METHODS OF FLOW INVESTIGATION, 2006, 6262
  • [27] Open-system pressure sensitive paint for surface pressure measurements in a cryogenic wind tunnel
    Sch. of Aeronautics and Astronautics, Purdue University, West Lafayette, IN, United States
    ICIASF Rec Int Congr Instrum Aerosp Simul Facil, 1600, (186-195):
  • [28] Open-system pressure sensitive paint for surface pressure measurements in a cryogenic wind tunnel
    Sakaue, H
    Sullivan, JP
    Egami, Y
    Iijima, Y
    Asai, K
    Engler, RH
    Beifuss, U
    Döring, F
    ICIASF'01: 19TH INTERNATIONAL CONGRESS ON INSTRUMENTATION IN AEROSPACE SIMULATION FACILITIES, RECORD, 2001, : 186 - 195
  • [29] Pressure sensitive paint in transonic wind-tunnel testing of the F-15
    Dowgwillo, RM
    Morris, MJ
    Donovan, JF
    Benne, ME
    JOURNAL OF AIRCRAFT, 1996, 33 (01): : 109 - 116
  • [30] Experimental technique of pressure sensitive paint based on 0.6 m trisonic wind tunnel
    Liu X.
    Xiong J.
    Huang H.
    Li Y.
    Huang Y.
    Wang H.
    Chen Z.
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2020, 41 (07):
12345