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Fluorescence spectroscopy and thermometry for hypersonic flight researchThe present study, which has demonstrated the feasibility of using time-resolved laser-induced fluorescence methods to ascertain boundary layer temperature distributions in real time for hypersonic vehicles in atmospheric flight, employs conventional optics in combination with novel time-resolved spectroscopy. The radiative lifetime and signal intensity involved, both of which are reduced by quenching, are adequate for measurement with state-of-the-art time-resolved fluorescence techniques, except for certain conditions associated with both the highest speeds and the lowest altitudes.
Document ID
19900046842
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Thompson, B. E.
(Scientific Research Associates, Inc. Glastonbury, CT, United States)
Fernandez, S. M.
(Scientific Research Associates, Inc. Glastonbury, CT, United States)
Guignon, E. F.
(Scientific Research Associates, Inc. Glastonbury, CT, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Instrumentation And Photography
Report/Patent Number
AIAA PAPER 90-1272
Report Number: AIAA PAPER 90-1272
Meeting Information
Meeting: AIAA/SFTE/DGLR/SETP Biannual Flight Test Conference
Location: Ontario, CA
Country: United States
Start Date: May 22, 1990
End Date: May 24, 1990
Accession Number
90A33897
Funding Number(s)
CONTRACT_GRANT: NAS1-18804
Distribution Limits
Public
Copyright
Other

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