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
  • [21] Luminescence lifetime response of pressure-sensitive paint to a pressure transient
    Drouillard, TF
    Linne, MA
    AIAA JOURNAL, 2005, 43 (05) : 1100 - 1108
  • [22] Pressure-sensitive paint measurement of pressure distribution in a supersonic micronozzle
    Nagai, H.
    Naraoka, R.
    Sawada, K.
    Asai, K.
    AIAA JOURNAL, 2008, 46 (01) : 215 - 222
  • [23] Blade Tip Pressure Measurements Using Pressure-Sensitive Paint
    Wong, Oliver D.
    Watkins, A. Neal
    Goodman, Kyle Z.
    Crafton, Jim
    Forlines, Alan
    Goss, Larry
    Gregory, James W.
    Juliano, Thomas J.
    JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 2018, 63 (01)
  • [24] Pressure-sensitive paint measurement of pressure distribution in a supersonic micronozzle
    Nagai, H.
    Naraoka, R.
    Sawada, K.
    Asai, K.
    AIAA Journal, 2008, 46 (01): : 215 - 222
  • [25] Sound-source distribution in the bogie section of a train determined by simultaneous measurement by pressure-sensitive paint and a microphone
    Matsui, Akitoshi
    Kasai, Miku
    Sugioka, Yosuke
    Asai, Keisuke
    Nonomura, Taku
    EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2023, 145
  • [26] Ultrafast pressure-sensitive paint for shock compression spectroscopy
    Banishev, Alexandr A.
    Dlott, Dana D.
    JOURNAL OF APPLIED PHYSICS, 2014, 115 (20)
  • [27] Optimum thickness of pressure-sensitive paint for unsteady measurements
    Schairer, ET
    AIAA JOURNAL, 2002, 40 (11) : 2312 - 2318
  • [28] Comparison of Unsteady Pressure-Sensitive Paint Measurement Techniques
    Fang, Shuo
    Long, Samuel R.
    Disotell, Kevin J.
    Gregory, James W.
    Semmelmayer, Frank C.
    Guyton, Robert W.
    AIAA JOURNAL, 2012, 50 (01) : 109 - 122
  • [29] Application of pressure-sensitive paint in supersonic nozzle research
    Cler, D
    Lamb, M
    Farokhi, S
    Taghavi, R
    Hazlewood, R
    JOURNAL OF AIRCRAFT, 1996, 33 (06): : 1109 - 1114
  • [30] Porous pressure-sensitive paint for characterizing unsteady flowfields
    Sakaue, H
    Gregory, JW
    Sullivan, JR
    Raghu, S
    AIAA JOURNAL, 2002, 40 (06) : 1094 - 1098