NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
The effect of incomplete fuel-air mixing on the lean limit and emissions characteristics of a Lean Prevaporized Premixed (LPP) combustorResults are presented from an experimental study of the effect of incomplete fuel-air mixing on the lean limit and emissions characteristics of a lean, prevaporized, premixed (LPP), coaxial mixing tube combustor. Two-dimensional exciplex fluorescence was used to characterize the degree of fuel vaporization and mixing at the combustor inlet under non-combusting conditions. These tests were conducted at a pressure of 4 atm., a temperature of 400 C, a mixer tube velocity of 100 m/sec and an equivalence ratio of .8, using a mixture of tetradecane, 1 methyl naphthalene and TMPD as a fuel simulant. Fuel-air mixtures with two distinct spatial distributions were studied. The exciplex measurements showed that there was a significant amount of unvaporized fuel at the combustor entrance in both cases. One case, however, exhibited a very non-uniform distribution of fuel liquid and vapor at the combustor entrance, i.e., with most of the fuel in the upper half of the combustor tube, while in the other case, both the fuel liquid and vapor were much more uniformly distributed across the width of the combustor entrance. The lean limit and emissions measurements were all made at a pressure of 4 atm. and a mixer tube velocity of 100 m/sec, using Jet A fuel and both fuel-air mixture distributions. Contrary to what was expected, the better mixed case was found to have a substantially leaner operating limit. The two mixture distributions also unexpectedly resulted in comparable NO(x) emissions, for a given equivalence ratio and inlet temperature, however, lower NO(x) emissions were possible in the better mixed case due to its leaner operating limit.
Document ID
19940024762
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
D. A. Santavicca
(Pennsylvania State Univ. University Park, PA, United States)
R. L. Steinberger
(Pennsylvania State Univ. University Park, PA, United States)
K. A. Gibbons
(Pennsylvania State Univ. University Park, PA, United States)
J. V. Citeno
(Pennsylvania State Univ. University Park, PA, United States)
S. Mills
(Pennsylvania State Univ. University Park, PA, United States)
Date Acquired
August 16, 2013
Publication Date
September 1, 1993
Publication Information
Publication: AGARD, Fuels and Combustion Technology for Advanced Aircraft Engines
Publisher: North Atlantic Treaty Organization
ISBN: 92-835-0719-3
Subject Category
Inorganic And Physical Chemistry
Report/Patent Number
AGARD-CP-536
AD-A275679
Meeting Information
Meeting: The Propulsion and Energetics Panel 81st Symposium
Location: Fiuggi
Country: IT
Start Date: May 10, 1993
End Date: May 14, 1993
Sponsors: North Atlantic Treaty Organization
Accession Number
94N29265
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Document Inquiry

Available Downloads

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