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Development of advanced diagnostics for characterization of burning droplets in microgravityDiagnostic techniques currently used for microgravity research are generally not as advanced as those used in earth based gravity experiments. Diagnostic techniques for measuring the instantaneous radial temperature profile (or temperature gradients) within the burning droplet do not exist. Over the past few years, Aerometrics has been researching and developing a rainbow thermometric technique for measuring the droplet temperatures of burning droplets. This technique has recently been integrated with the phase Doppler interferometric technique to yield a diagnostic instrument that can be used to simultaneously measure the size, velocity, and temperature of burning droplets in complex spray flames. Also, the rainbow thermometric technique has been recently integrated with a point-diffraction interferometric technique for measuring the instantaneous gas phase temperature field surrounding a burning droplet. These research programs, apart from being very successful, have also helped us identify other innovative techniques for the characterization of burning droplets. For example, new techniques have been identified for measuring the instantaneous regression rate of burning droplets. Also, there is the possibility of extracting the instantaneous radial temperature distribution or the temperature gradients within a droplet during transient heating. What is important is that these diagnostic techniques have the potential for making use of inexpensive, light-weight, and rugged devices such as diode lasers and linear CCD arrays. As a result, they can be easily packaged for incorporation into microgravity drop-test and flight-test facilities. Furthermore, with the use of linear CCD arrays, data rates as high as 10-100 kHz can be easily achieved. This data rate is orders of magnitude higher than what is currently achievable. In this research and development program, a compact and rugged diagnostic system will be developed that can be used to measure instantaneous fuel droplet diameter, droplet regression rate, and the droplet internal temperature profiles or gradients at very high data rates in microgravity experiments.
Document ID
19960008428
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sankar, Subramanian
(Aerometrics, Inc. Sunnyvale, CA, United States)
Buermann, Dale H.
(Aerometrics, Inc. Sunnyvale, CA, United States)
Bachalo, William D.
(Aerometrics, Inc. Sunnyvale, CA, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1995
Publication Information
Publication: NASA. Lewis Research Center, The 3rd International Microgravity Combustion Workshop
Subject Category
Materials Processing
Accession Number
96N15594
Funding Number(s)
CONTRACT_GRANT: NAS3-27261
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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