Open-system pressure sensitive paint for surface pressure measurements in a cryogenic wind tunnel

被引:0
|
作者
Sch. of Aeronautics and Astronautics, Purdue University, West Lafayette, IN, United States [1 ]
机构
关键词
Compendex;
D O I
19th International Congress on Instrumentation in Aerospace Simulation Facilities (ICIASF 2001)
中图分类号
学科分类号
摘要
Anodic oxidation - Calibration - Cryogenics - Pressure measurement - Surface properties - Wind tunnels
引用
收藏
相关论文
共 50 条
  • [1] 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
  • [2] Time-resolved pressure-sensitive paint measurements for cryogenic wind tunnel tests
    Yorita D.
    Henne U.
    Klein C.
    CEAS Aeronautical Journal, 2024, 15 (01) : 37 - 47
  • [3] Pressure-sensitive paint measurements in a blowdown wind tunnel
    Raju, C
    Viswanath, PR
    JOURNAL OF AIRCRAFT, 2005, 42 (04): : 908 - 915
  • [4] Pressure-sensitive paint technique for surface pressure measurements in a low-density wind tunnel
    Anyoji, M.
    Numata, D.
    Nagai, H.
    Asai, K.
    JOURNAL OF VISUALIZATION, 2015, 18 (02) : 297 - 309
  • [5] Pressure-sensitive paint technique for surface pressure measurements in a low-density wind tunnel
    M. Anyoji
    D. Numata
    H. Nagai
    K. Asai
    Journal of Visualization, 2015, 18 : 297 - 309
  • [6] Novel pressure-sensitive paint for cryogenic and unsteady wind-tunnel testing
    Asai, K
    Amao, Y
    Iijima, Y
    Okura, I
    Nishide, H
    JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER, 2002, 16 (01) : 109 - 115
  • [7] Hysteresis of pressure-sensitive paint in cryogenic wind tunnels
    Egami Y.
    Iijima Y.
    Asai K.
    Nihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B, 2010, 76 (762): : 254 - 258
  • [8] Pressure sensitive paint measurements on a wing model in a low-speed wind tunnel
    Klein, C
    Engler, RH
    Fonov, SD
    Trinks, O
    ICIASF'99: INTERNATIONAL CONGRESS ON INSTRUMENTATION IN AEROSPACE SIMULATION FACILITIES, RECORD, 1999, : 221 - 226
  • [9] Surface Pressure Measurements on a Forebody Using Pressure Sensitive Paint
    Chung, K. M.
    Huang, Y. X.
    Lin, C. Y.
    Wu, Y. T.
    JOURNAL OF AERONAUTICS ASTRONAUTICS AND AVIATION, 2021, 53 (03): : 369 - 374
  • [10] Pressure sensitive paint systems for pressure distribution measurements in wind tunnels and turbomachines
    Engler, RH
    Klein, C
    Trinks, O
    MEASUREMENT SCIENCE AND TECHNOLOGY, 2000, 11 (07) : 1077 - 1085