NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Odor intensity and characterization studies of exhaust from a turbojet engine combustorSensory odor tests of the exhaust from a turbojet combustor operating at simulated idle conditions were made by a human panel sniffing diluted exhaust gas. Simultaneously, samples of undiluted exhaust gas were collected on adsorbent substrates, subsequently removed by solvent flushing, and analyzed chemically by liquid chromatographic methods. The concentrations of the principal malodorous species, the aromatic (unburned fuel-related) and the oxygenated (partially burned fuel) fractions, as determined chromatographically, correlated well with the intensity of the odor as determined by sniffing. Odor intensity increased as combustion efficiency decreased. Combustor modifications which increased combustion efficiency decreased odor intensity.
Document ID
19740028540
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Butze, H. F.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Kendall, D. A.
(NASA Lewis Research Center Cleveland, Ohio; Arthur D. Little, Inc., Cambridge, Mass., United States)
Date Acquired
August 7, 2013
Publication Date
November 1, 1973
Subject Category
Facilities, Research, And Support
Report/Patent Number
AIAA PAPER 73-1278
Meeting Information
Meeting: Propulsion Conference
Location: Las Vegas, NV
Country: US
Start Date: November 5, 1973
End Date: November 7, 1973
Sponsors: Society of Automotive Engineers, American Institute of Aeronautics and Astronautics
Accession Number
74A11290
Distribution Limits
Public
Copyright
Other

Available Downloads

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