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Advanced instrumentation for aircraft icing researchA compact and rugged probe based on the phase Doppler method was evaluated as a means for characterizing icing clouds using airborne platforms and for advancing aircraft icing research in large scale wind tunnels. The Phase Doppler Particle Analyzer (PDPA) upon which the new probe was based is now widely recognized as an accurate method for the complete characterization of sprays. The prototype fiber optic-based probe was evaluated in simulated aircraft icing clouds and found to have the qualities essential to providing information that will advance aircraft icing research. Measurement comparisons of the size and velocity distributions made with the standard PDPA and the fiber optic probe were in excellent agreement as were the measurements of number density and liquid water content. Preliminary testing in the NASA Lewis Icing Research Tunnel (IRT) produced reasonable results but revealed some problems with vibration and signal quality at high speeds. The cause of these problems were identified and design changes were proposed to eliminate the shortcomings of the probe.
Document ID
19900011690
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bachalo, W.
(Aerometrics, Inc. Sunnyvale, CA, United States)
Smith, J.
(Aerometrics, Inc. Sunnyvale, CA, United States)
Rudoff, R.
(Aerometrics, Inc. Sunnyvale, CA, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1990
Subject Category
Aircraft Instrumentation
Report/Patent Number
NASA-CR-185225
NAS 1.26:185225
Report Number: NASA-CR-185225
Report Number: NAS 1.26:185225
Accession Number
90N21006
Funding Number(s)
PROJECT: RTOP 505-68-11
CONTRACT_GRANT: NAS3-25317
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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