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Dual-Mode Scramjet Flameholding Operability MeasurementsFlameholding measurements were made in two different direct connect combustor facilities that were designed to simulate a cavity flameholder in the flowfield of a hydrocarbon fueled dual-mode scramjet combustor. The presence of a shocktrain upstream of the flameholder has a significant impact on the inlet flow to the combustor and on the flameholding limits. A throttle was installed in the downstream end of the test rigs to provide the needed back-pressurization and decouple the operation of the flameholder from the backpressure formed by heat release and thermal choking, as in a flight engine. Measurements were made primarily with ethylene fuel but a limited number of tests were also performed with heated gaseous JP-7 fuel injection. The flameholding limits were measured by ramping inlet air temperature down until blowout was observed. The tests performed in the United Technologies Research Center (UTRC) facility used a hydrogen fueled vitiated air heater, Mach 2.2 and 3.3 inlet nozzles, a scramjet combustor rig with a 1.666 by 6 inch inlet and a 0.65 inch deep cavity. Mean blowout temperature measured at the baseline condition with ethylene fuel, the Mach 2.2 inlet and a cavity pressure of 21 psia was 1502 oR. Flameholding sensitivity to a variety of parameters was assessed. Blowout temperature was found to be most sensitive to fuel injection location and fuel flowrates and surprisingly insensitive to operating pressure (by varying both back-pressurization and inlet flowrate) and inlet Mach number. Video imaging through both the bottom and side wall windows was collected simultaneously and showed that the flame structure was quite unsteady with significant lateral movements as well as movement upstream of the flameholder. Experiments in the University of Virginia (UVa) test facility used a Mach 2 inlet nozzle with a 1 inch by 1.5 inch exit cross section, an aspect ratio of 1.5 versus 3.6 in the UTRC facility. The UVa facility tests were designed to measure the sensitivity of flameholding limits to inlet air vitiation by using electrically heated air and adding steam at levels to simulate vitiated air heaters. The measurements showed no significant difference in blowout temperature with inlet air mole fractions of steam from 0 to 6.7%.
Document ID
20140005746
Acquisition Source
Glenn Research Center
Document Type
Contractor or Grantee Report
Authors
Donohue, James M.
(United Technologies Research Center East Hartford, CT, United States)
Date Acquired
May 13, 2014
Publication Date
September 30, 2012
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-TN10262
Report Number: GRC-E-DAA-TN10262
Funding Number(s)
CONTRACT_GRANT: NNC08CA79C
WBS: WBS 475122.02.07.09.01
WBS: WBS 599489.02.07.03.11.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
airbreathing engines aircraft
combustors aircraft
scramjet engines aircraft
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