Pressure-sensitive paint as a distributed optical microphone array

被引:36
|
作者
Gregory, JW [1 ]
Sullivan, JP
Wanis, SS
Komerath, NM
机构
[1] Purdue Univ, Sch Aeronaut & Astronaut, W Lafayette, IN 47907 USA
[2] Georgia Inst Technol, Sch Aerosp Engn, Atlanta, GA 30332 USA
来源
基金
美国国家航空航天局;
关键词
D O I
10.1121/1.2140935
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
Pressure-sensitive paint is presented and evaluated in this article as a quantitative technique for measurement of acoustic pressure fluctuations. This work is the culmination of advances in paint technology which enable unsteady measurements of fluctuations over 10 kHz at pressure levels as low as 125 dB. Pressure-sensitive paint may be thought of as a nano-scale array of optical microphones with a spatial resolution limited primarily by the resolution of the imaging device. Thus, pressure-sensitive paint is a powerful tool for making high-amplitude sound pressure measurements. In this work, the paint was used to record ensemble-averaged, time-resolved, quantitative measurements of two-dimensional mode shapes in an acoustic resonance cavity. A wall-mounted speaker generated nonlinear, standing acoustic waves in a rigid enclosure measuring 216 mm wide, 169 mm high, and 102 mm deep. The paint recorded the acoustic surface pressures of the (1,1,0) mode shape at similar to 1.3 kHz and a sound pressure level of 145.4 dB. Results from the paint are compared with data from a Kulite pressure transducer, and with linear acoustic theory. The paint may be used as a diagnokic technique for ultrasonic tests where high spatial resolution is essential, or in nonlinear acoustic applications such as shock tubes. (c) 2006 Acoustical Society of America.
引用
收藏
页码:251 / 261
页数:11
相关论文
共 50 条
  • [41] 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
  • [42] Pressure-Sensitive Paint Measurements of Transient Shock Phenomena
    Quinn, Mark Kenneth
    Kontis, Konstantinos
    SENSORS, 2013, 13 (04): : 4404 - 4427
  • [43] Reduction of Temperature Effects in Pressure-Sensitive Paint Measurements
    Egami, Y.
    Fujii, K.
    Takagi, T.
    Matsuda, Y.
    Yamaguchi, H.
    Niimi, T.
    AIAA JOURNAL, 2013, 51 (07) : 1779 - 1783
  • [44] Shock-dominated flow control by plasma array: Pressure analysis including pressure-sensitive paint visualization
    Elliott, Skye
    Hasegawa, Mitsugu
    Sakaue, Hirotaka
    Leonov, Sergey
    EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2022, 131
  • [45] Optical measurements of high-frequency pressure fluctuations using a pressure-sensitive paint and Cassegrain optics
    Sakamura, Y
    Suzuki, T
    Matsumoto, M
    Masuya, G
    Ikeda, Y
    MEASUREMENT SCIENCE AND TECHNOLOGY, 2002, 13 (10) : 1591 - 1598
  • [46] PRESSURE FIELD MEASUREMENT ON COMPRESSOR CASCADE USING PRESSURE-SENSITIVE PAINT
    Gao, Limin
    Hu, Xiaoquan
    Tian, Linchuan
    Li, Ruiyu
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2016, VOL 2A, 2016,
  • [47] On the Use of Pressure-Sensitive Paint to Determine the Rim Sealing Effectiveness
    Orsini, L.
    Picchi, A.
    Facchini, B.
    Bonini, A.
    Innocenti, L.
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2024, 146 (02):
  • [48] Use of pressure-sensitive paint for diagnostics in turbomachinery flows with shocks
    J. Lepicovsky
    T. Bencic
    Experiments in Fluids, 2002, 33 : 531 - 538
  • [49] Limiting Mach number for quantitative pressure-sensitive paint measurements
    Mendoza, DR
    AIAA JOURNAL, 1997, 35 (07) : 1240 - 1241
  • [50] Techniques for using pressure-sensitive paint in shock tunnel facilities
    Hubner, JP
    Carroll, BF
    Schanze, KS
    Ji, HF
    ICIASF '97 RECORD - INTERNATIONAL CONGRESS ON INSTRUMENTATION IN AEROSPACE SIMULATION FACILITIES, 1997, : 30 - 39