Research Catalog

New! Try our Article Search to discover online journals, books, and more from home with your library card.

Selected filters.Clear Filters

  • Stratified charge rotary engine critical technology enablement. Volume I [microform] / C.E. Irion and R.E. Mount.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Stratified charge rotary engine critical technology enablement. Volume II, Appendixes [microform] / C.E. Irion and R.E. Mount.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Zero-G Thermodynamic Venting System (TVS) performance prediction program [microform] / prepared by Han Nguyen.

    • Text
    • Downey, Calif. : Rockwell Aerospace ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Investigation of ramp injectors for supersonic mixing enhancement [microform] / Y. Haimovitch, E. Gartenberg, and A.S. Roberts.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, VA : National Technical Information Service, distributor, 1994]
    • 1994

  • Fuel-injector/air-swirl characterization [microform] / J.B. McVey, J.B. Kennedy and S. Russell.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1988]
    • 1988

  • Role of fuel chemical properties on combustor radiative heat load [microform] / T.J. Rosfjord.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1984]
    • 1984

  • Shock tunnel studies of scramjet phenomena 1993 [microform] : supplement 10 / R.J. Stalker ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Propellant injection systems and processes [microform] / Jackson I. Ito.

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

  • Stratified charge rotary engine combustion studies [microform] : progress report / principal investigator, H. Schock, co-investigators R. Hamady and C. Somerton.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Scramjet sidewall burning, preliminary shock tunnel results, NASA contract no. NAGW-674 [microform] / by R.G. Morgan ... [et al.].

    • Text
    • [Brisbane, Australia] : University of Queensland, Dept. of Mechanical Engineering ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Performance of a low-power subsonic-arc-attachment arcjet thruster [microform] / John M. Sankovic and Darren H. Berns.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • Two rotor stratified charge rotary engine (SCRE) engine system technology evaluation [microform] / T. Hoffman, J. Mack, and R. Mount.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • A unique, optically accessible flame tube facility for lean combustor studies [microform] / Yolanda R. Hicks ... [et al.].

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

  • Advanced diesel engine component development program [microform] : final report, tasks 4-14 / Tony S. Kaushal, Karen E. Weber.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration] ; Springfield, VA : Available from the National Technical Information Service, [1994]
    • 1994

  • NASA flow field analysis [microform] : final report / Charles L. Merkle.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Construction of a direct water-injected two-stroke engine for phased direct fuel injection-high pressure charging investigations [microform] : order number, A49222D (LAS), April 1, 1998 / prepared by Orbital Engine Company (USA) Inc.

    • Text
    • Tecumseh, MI : Orbital Engine Company (USA) Inc. ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Atomization and dispersion of a liquid jet injected into a crossflow of air [microform] : under grant NAG3-1124 / J.E. Seay and G.S. Samuelsen.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Comparison of techniques for non-intrusive fuel drop size measurements in a subscale gas turbine combustor [microform] / Michelle Zaller ... [et al.].

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • Effect of jet injection angle and number of jets on mixing and emissions from a reacting crossflow at atmospheric pressure [microform] / D. St. John and G. S. Samuelsen.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : National Technical Information Service, distributor, [2000]
    • 2000

  • Flame tube NOx emissions using a lean-direct-wall-injection combustor concept [microform] / Robert R. Tacina, Changlie Wey, Kyung J. Choi.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS27505

  • Spontaneous raman scattering [microform] : from atmospheric CH4/air diffusion flame to 55 bar jet-a-fueled, aviation gas turbine combustor / R.J. Locke ... [et al.].

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2002]
    • 2002

  • A design methodology for rapid implementation of active control systems across lean direct injection combustor platforms [microform] / William T. Baumann, William R. Saunders, and Uri Vandsburger.

    • 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, 2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS55120

  • Fuel injector design optimization for an annular scramjet geometry [microform] / Christopher J. Steffen, Jr.

    • Text
    • [Cleveland, Ohio : NASA Glenn Research Center, 2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS56848

  • 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

  • Two-dimensional analysis of two-phase reacting flow in a firing direct-injection diesel engine [microform] / H. Lee Nguyen.

    • 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/LPS61317

  • Analysis of rotary engine combustion processes based on unsteady, three-dimensional computations [microform] / M.S. Raju and E.A. Willis ; prepared for the 28th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Reno, Nevada, January 8-11.

    • 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/LPS70013

  • Aerodynamic effect of combustor inlet-air pressure on fuel jet atomization [microform] / Robert D. Ingebo.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1984]
    • 1984

  • Lightweight two-stroke cycle aircraft diesel engine technology enablement program [microform] : final report / P.D. Freen ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Office, [1985]
    • 1985

  • Flame propagation in heterogeneous mixtures of fuel drops and air [microform] / G.D. Myers and A.H. Lefebvre.

    • Text
    • [West Lafayette, Ind.] : Purdue University, [1984]
    • 1984

  • Atomization and mixing study / prepared by A. Ferrenberg, K. Hunt, J. Duesberg.

    • Text
    • Canoga Park, Calif. : Roclwell International, Rocketdyne Division ; Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1985]
    • 1985
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24414

  • Atomization and mixing study [microform] / prepared by A. Ferrenberg, K. Hunt, J. Duesberg.

    • Text
    • Canoga Park, Calif. : Roclwell International, Rocketdyne Division ; Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1985]
    • 1985

  • Effects of spent cooling and swirler angle on a 9-point swirl-venturi injector / Zhuohui J. He [and four others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2014.
    • 2014-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo54279

  • Fundamental study of a single point lean direct injector part I : effect of air swirler angle and injector tip location on spray characteristics / Sarah A. Tedder [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, February 2015.
    • 2015-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo57559

  • Low-pressure performance of annular, high-pressure (40-atm), high-temperature, (2480 K) combustion system / Jerrold D. Wear, Arthur M. Trout, and John M. Smith.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, September 1980.
    • 1980-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71101

  • Capillary and acceleration wave breakup of liquid jets in axial-flow airstreams / Robert D. Ingebo.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, January 1981.
    • 1981-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71446

  • Performance of semi-transpiration-cooled liner in high-temperature-rise combustor / Jerrold D. Wear, Arthur M. Trout and John M. Smith.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, March 1981.
    • 1981-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71512

  • NOx emissions characteristics and correlation equations of two P & W's axially staged sector combustors developed under NASA Environmentally Responsible Aviation (ERA) project / Zhuohui J. He.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, January 2017.
    • 2017-1
    • 2 Resources

    Available Online

    See All Available Online Resources

  • Fuel injector design optimization for an annular scramjet geometry / Christopher J. Steffen, Jr.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, January 2003.
    • 2003-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS56848

  • Investigations of a combustor using a 9-point swirl-venturi fuel injector : recent experimental results / Yolanda R. Hicks ... [and others].

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo29172

  • Performance evaluation of a high bandwidth liquid fuel modulation valve for active combustion control / Joseph R. Saus [and three others].

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo33032

  • NASA numerical and experimental evaluation of UTRC low emissions injector / Yolanda R. Hicks [and five others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2014.
    • 2014-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo56698

No results found from Digital Research Books Beta

Digital books for research from multiple sources world wide- all free to read, download, and keep. No Library Card is Required. Read more about the project.

digital-research-book
Explore Digital Research Books Beta