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  • Aircraft Propulsion and Power  (3)
  • 2005-2009  (3)
  • 1
    Publication Date: 2019-07-13
    Description: This paper discusses the progress of work which began in mid-2004 sponsored by the Office of the Secretary of Defense (OSD) Test & Evaluation/Science & Technology (T&E/S&T) Program. The purpose of the work is to improve the state of the art of CFD capabilities for predicting the effects of the test media on the flameholding characteristics in scramjet engines. The program has several components including the development of advance algorithms and models for simulating engine flowpaths as well as a fundamental experimental and diagnostic development effort to support the formulation and validation of the mathematical models. The paper will provide details of current work involving the development of phenomenological models for Reynolds averaged Navier-Stokes codes, large-eddy simulation techniques and reduced-kinetics models. Experiments that will provide data for the modeling efforts will also be described, along with with the associated nonintrusive diagnostics used to collect the data.
    Keywords: Aircraft Propulsion and Power
    Type: 2006 Annual ITEA Technology Review; Aug 07, 2006 - Aug 10, 2006; Cambridge, MA; United States
    Format: application/pdf
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  • 2
    Publication Date: 2019-07-13
    Description: This paper discusses the progress of work to model high-speed supersonic reacting flow. The purpose of the work is to improve the state of the art of CFD capabilities for predicting the flow in high-speed propulsion systems, particularly combustor flowpaths. The program has several components including the development of advanced algorithms and models for simulating engine flowpaths as well as a fundamental experimental and diagnostic development effort to support the formulation and validation of the mathematical models. The paper will provide details of current work on experiments that will provide data for the modeling efforts along with the associated nonintrusive diagnostics used to collect the data from the experimental flowfield. Simulation of a recent experiment to partially validate the accuracy of a combustion code is also described.
    Keywords: Aircraft Propulsion and Power
    Type: 2007 Fall Technical Meeting - Eastern States Section of the Combustion Institute; Oct 21, 2007 - Oct 24, 2007; Charlotesville, VA; United States
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  • 3
    Publication Date: 2019-07-13
    Description: The coherent anti-Stokes Raman spectroscopy (CARS) method has recently been used in the United States and Europe to probe several different types of propulsion systems for air vehicles. At NASA Langley Research Center in the United States, CARS has been used to simultaneously measure temperature and the mole fractions of N2, O2 and H2 in a supersonic combustor, representative of a scramjet engine. At Wright- Patterson Air Force Base in the United States, CARS has been used to simultaneously measure temperature and mole fractions of N2, O2 and CO2, in the exhaust stream of a liquid-fueled, gas-turbine combustor. At ONERA in France and the DLR in Germany researchers have used CARS to measure temperature and species concentrations in cryogenic LOX-H2 rocket combustion chambers. The primary aim of these measurements has been to provide detailed flowfield information for computational fluid dynamics (CFD) code validation.
    Keywords: Aircraft Propulsion and Power
    Type: RTO-MP-AVT-124-Paper 5 , LF99-1354 , RTO/AVT-124 Specialists Meeting on Recent Developments in Non-Intrusive Measurement Technology for Military Application on Model-and Full-Scale Vehicles; Apr 25, 2005 - Apr 29, 2005; Budapest; Hungary
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