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Conjugate Heat Transfer Analyses on the Manifold for Ramjet Fuel InjectorsThree-dimensional conjugate heat transfer analyses on the manifold located upstream of the ramjet fuel injector are performed using CFdesign, a finite-element computational fluid dynamics (CFD) software. The flow field of the hot fuel (JP-7) flowing through the manifold is simulated and the wall temperature of the manifold is computed. The three-dimensional numerical results of the fuel temperature are compared with those obtained using a one-dimensional analysis based on empirical equations, and they showed a good agreement. The numerical results revealed that it takes around 30 to 40 sec to reach the equilibrium where the fuel temperature has dropped about 3 F from the inlet to the exit of the manifold.
Document ID
20060056390
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Wang, Xiao-Yen J.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
November 1, 2006
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NASA/TM-2006-214455
E-15719
TFAWS06-1036
Report Number: NASA/TM-2006-214455
Report Number: E-15719
Report Number: TFAWS06-1036
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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