NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Optical Imaging of Flow Pattern and PhantomTime-resolved optical imaging technique has been used to image the spatial distribution of small droplets and jet sprays in a highly scattering environment. The snake and ballistic components of the transmitted pulse are less scattered, and contain direct information about the sample to facilitate image formation as opposed to the diffusive components which are due to multiple collisions as a light pulse propagates through a scattering medium. In a time-gated imaging scheme, these early-arriving, image-bearing components of the incident pulse are selected by opening a gate for an ultrashort period of time and a shadowgram image is detected. Using a single shot cooled CCD camera system, the formation of water droplets is monitored as a function of time. Picosecond time-gated image of drop in scattering cells, spray droplets as a function of let speed and gas pressure, and model calcification samples consisted of calcium carbonate particles of irregular shapes ranging in size from 0. 1 to 1.5 mm affixed to a microscope slide have been measured. Formation produced by an impinging jet will be further monitored using a CCD with 1 kHz framing illuminated with pulsed light. The desired image resolution of the fuel droplets is on the 20 pm scale using early light through a highly scattering medium. A 10(exp -6)m displacement from a jet spray with a flow speed of 100 m/sec introduced by the ns grating pulse used in the imaging is negligible. Early ballistic/snake light imaging offers nondestructive and noninvasive method to observe the spatial distribution of hidden objects inside a highly scattering environment for space, biomedical, and materials applications. In this paper, the techniques we will present are time-resolved K-F transillumination imaging and time-gated scattered light imaging. With a large dynamic range and high resolution, time-gated early light imaging has the potential for improving rocket/aircraft design by determining jets shape and particle sizes. Refinements to these techniques may enable drop size measurements in the highly scattering, optically dense region of multi-element rocket injectors. These types of measurements should greatly enhance the design of stable, and higher performing rocket engines.
Document ID
19990111485
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Galland, Pierre A.
(City Coll. of the City Univ. of New York NY United States)
Liang, X.
(City Coll. of the City Univ. of New York NY United States)
Wang, L.
(City Coll. of the City Univ. of New York NY United States)
Ho, P. P.
(City Coll. of the City Univ. of New York NY United States)
Alfano, R. R.
(City Coll. of the City Univ. of New York NY United States)
Breisacher, K.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
August 19, 2013
Publication Date
August 1, 1999
Publication Information
Publication: HBCUs/OMUs Research Conference Agenda and Abstracts
Subject Category
Optics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

There are no available downloads for this record.
No Preview Available