NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Filtered Mass Density Function for Design Simulation of High Speed Airbreathing Propulsion SystemsThe objective of this research is to improve and implement the filtered mass density function (FDF) methodology for large eddy simulation (LES) of high speed reacting turbulent flows. NASA is interested in the design of various components involved in air breathing propulsion systems such as the scramjet. There is a demand for development of robust tools that can aid in the design procedure. The physics of high speed reactive flows is rich with many complexities. LES is regarded as one of the most promising means of simulating turbulent reacting flows.
Document ID
20020066763
Acquisition Source
Langley Research Center
Document Type
Contractor or Grantee Report
Authors
Givi, P.
(State Univ. of New York Buffalo, NY United States)
Madnia, C. K.
(State Univ. of New York Buffalo, NY United States)
Gicquel, L. Y. M.
(State Univ. of New York Buffalo, NY United States)
Sheikhi, M. R. H.
(State Univ. of New York Buffalo, NY United States)
Drozda, T. G.
(State Univ. of New York Buffalo, NY United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Aircraft Propulsion And Power
Funding Number(s)
CONTRACT_GRANT: NAG1-2238
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available