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  • A sectored-one-dimensional model for simulating combustion instabilities in premix combustors [microform] / Daniel E. Paxson.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information ; Springfield, VA : National Technical Information Service [distributor, 1999]
    • 1999

  • Advanced CFD methodology for fast transients encountered in nonlinear combustion instability problems [microform] : SBIR phase II final report (restricted circulation) / by H.Q. Yang ... [et al.].

    • Text
    • [Marshall Space Flight Center, Ala.] : National Aeronautics and Space Administration, George C. Marshall Space Flight Center ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Flow diagnostics, chemically reacting turbulent flow modeling and turbulent mixing [microform] : a summary of project studies in combustion / principal investigator: Bahman Ghorashi.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Sensitivity of combustion-acoustic instabilities to boundary conditions for premixed gas turbinecombustors [microform] / Douglas darling, Krishnan Radhakrishnan, Ayo Oyediran.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • A fully implicit time accurate method for hypersonic combustion [microform] : application to shock-induced combustion instability / Shaye Yungster and Krishnan Radhakrishnan.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, Ohio Aerospace Institute, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Solid-propellant rocket motor internal ballistics performance variatio analysis (phase five) [microform] : final report / by Richard H. Sforzini and Jesse E. Murph.

    • Text
    • Auburn, Ala. : Engineering Experiment Station, Auburn University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1980]
    • 1980

  • Review of combustion-acoustic instabilities [microform] / Ayo Oyediran, Douglas Darling, Krishnan Radhakrishnan.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Combustion-acoustic stability analysis for premixed gas turbine combustors [microform] / Douglas Darling ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • ASRM combustion instability studies [microform] / L.D. Strand.

    • Text
    • [Pasadena, Calif.?] : Jet Propulsion Laboratory, California Institute of Technology ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Combustion noise at elevated pressures in a liquid-fueled premixed combustor [microform] / Douglas Darling, Krishnan Radhakrishnan, Ayo Oyediran.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Hybrid propulsion for launch vehicle boosters [microform] : a program status update / R.L. Carpenter, [et al.].

    • Text
    • Washington, D.C. : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Active combustion control for aircraft gas turbine engines [microform] / John C. DeLaat ... [et al.].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2000]
    • 2000
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS30202

  • A comparison of analytical results for 20 K LOX/hydrogen instabilities [microform] / Mark D. Klem and Kevin J. Breisacher ; prepared for the 26th Joint Propulsion Conference cosponsored by the AIAA, SAE, ASME, and ASEE, Orlando, Florida, July 16-18, 1990.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1990?]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS59891

  • LOX/Hydrocarbon combustion instability investigation [microform] / R.J. Jensen, H.C. Dodson, and S.E. Claflin.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS62256

  • Combustor flame flashback [microform] / Margaret P. Proctor and James S. T'ien.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1985]
    • 1985

  • Active combustion control for aircraft gas-turbine engines : experimental results for an advanced, low-emissions combustor prototype / John C. DeLaat ... [and others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo31847

  • High-speed linear Raman spectroscopy for instability analysis of a bluff body flame / Jun Kojima, David Fischer.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, January 2013.
    • 2013-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo51817

  • NASA one-dimensional combustor simulation : user manual for S1D_ML / Thomas J. Stueber and Daniel E. Paxson.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, October 2014.
    • 2014-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo57991

  • Combustion noise at elevated pressures in a liquid-fueled premixed combustor / Douglas Darling, Krishnan Radhakrishnan, Ayo Oyediran.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, June 1997.
    • 1997-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo79339

  • Active combustion control for aircraft gas turbine engines / John C. DeLaat [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2000.
    • 2000-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS30202

  • Nonsteady flame propagation. Edited by George H. Markstein.

    • Text
    • Oxford, New York, Published for and on behalf of Advisory Group for Aeronautical Research and Development, North Atlantic Treaty Organization by Pergamon Press; [distributed in the Western Hemisphere by Macmillan, New York] 1964.
    • 1964
    • 1 Item
    FormatCall NumberItem Location
    Text TL500 .N6 no.75Off-site

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