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OLS Field Name OLS Field Data
Main Title Nitric oxide measurement study : volume III : comparison of optical and probe methods /
Author Zabielski, M. F. ; Dodge, L. G. ; Colket, III, M. B. ; Seery, D. J. ;
Other Authors
Author Title of a Work
Zabielski, M. F.
CORP Author United Technologies Research Center, East Hartford, CT.;Federal Aviation Administration, Washington, DC. Office of Environment and Energy.;Environmental Protection Agency, Washington, DC.
Publisher Federal Aviation Administration, Office of Environment and Energy ; for sale by the National Technical Information Service,
Year Published 1980
Report Number USAF ESL TR-80-14; USN NAPC-PE-39C; EPA-460/3-80-015; R80-994150-3; DOT-FA77WA-4081; FAA-EE-80-30
Stock Number PB81-195547
OCLC Number 07470075
Subjects Ultraviolet spectroscopy. ; Gases at high temperatures. ; Aircraft exhaust emissions.
Additional Subjects Nitrogen oxide(NO) ; Air pollution ; Probes ; Optical measuring instruments ; Gas analysis ; Concentration(Composition) ; Comparison ; Exhaust emissions ; Sampling ; Burners ; Design criteria ; Aircraft ; Chemiluminescence ; Ultraviolet spectroscopy ; Air pollution detection ; NTISEPAMAP ; NTISDOTFAA ; NTISDODAF ; NTISNASA
Internet Access
Description Access URL
http://nepis.epa.gov/Exe/ZyPDF.cgi?Dockey=9100XM1S.PDF
Holdings
Library Call Number Additional Info Location Last
Modified
Checkout
Status
ELCD  EPA 460-3-80-015 NVFEL Library/Ann Arbor, MI 10/11/2011
NTIS  PB81-195547 Most EPA libraries have a fiche copy filed under the call number shown. Check with individual libraries about paper copy. NTIS 06/23/1988
Collation 95 p. in various pagings : ill. ; 28 cm.
Abstract
Nitric oxide (NO) was measured in the exhaust of three different combustion systems by in situ ultraviolet absorption and by chemiluminescent analysis after gas sampling with several probe designs. The three combustion systems were: (1) a flat flame burner fueled with CH4/N2/O2; (2) a research swirl burner fueled with C3H8/air; and, (3) a modified FT12 combustor operated on Jet A/air. Each combustion system was run at several different conditions so that probe and optical measurements could be obtained over a wide range of exhaust environments encompassing products from lean, stoichiometric, and rich flames, laminar to turbulent flows, and temperatures at centerline from 600 K to 1800 K. The results obtained with the metallic, water-cooled probes of different designs (all expansion-type) agreed with the optical results to within 25 percent. Some small losses of NO (10-15 percent) were observed in a lean methane flame at 1800 K with an uncooled stainless steel probe, but under fuel-rich conditions up to 80 percent NO destruction was observed. Experimental facilities are described, previous results are discussed, and a summary of the major findings of this study is given.
Notes
"March 31, 1980." "USAF ESL TR-80-14." "USN NAPC-PE-39C." "EPA-460/3-80-015." Contract no. DOT FA77WA-4081. Sponsored jointly by the Federal Aviation Administration, U.S. Air Force, U.S. Navy, National Aeronautics and Space Administration, and the Environmental Protection Agency. Includes bibliographical references.