Research Catalog

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  • The practical implementation of non-contacting laser strain measurement systems [microform] / Isam Yunis, Roger D. Quinn and Jaikrishnan R. Kadambi.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 2000]
    • 2000

  • Comparison of UNL laser imaging and sizing system and a phase Doppler system for analyzing sprays from a NASA nozzle [microform] / Dennis R. Alexander.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • Data reduction procedures for laser velocimeter measurements in turbomachinery rotors [microform] / Jan Lepicovsky.

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

  • Laser doppler velocimetry for continuous flow solar-pumped iodine laser system [microform] / Bagher M. Tabibi and Ja H. Lee.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, distributor, 1991]
    • 1991

  • High-temperature LDV seed particle development [microform] / Michael B. Frish and Vicky G. Pierce.

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

  • A three-dimensional orthogonal laser velocimeter for the NASA Ames 7- by 10-foot wind tunnel [microform] / Stephan E. Dunagan and Donald L. Cooper.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • 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

  • Experimental studies of vortex flows [microform] : final report, NASA grant NCC 2-294, report covering the period March 1984 - May 1988 / principal investigator, L. Roberts ; project leader, R. Mehta.

    • Text
    • Stanford, CA : Joint Institute for Aeronautics and Acoustics, Dept. of Aeronautics and Astronautics, Stanford University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • Coherent Raman spectroscopy for supersonic flow measurements [microform] : final report / principal investigator, C.Y. She.

    • Text
    • Fort Collins, Colo. : Dept. of Physics, Colorado State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1986

  • Wind tunnel seeding systems for laser velocimeters [microform] / compiled by William W. Hunter, Jr. and Cecil E. Nichols, Jr.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : for sale by the National Technical Information Service, 1985.
    • 1985

  • Conducting a wind sensing study [microform] : final technical report for the period December 31, 1983 to December 30, 1984 / principal ilnvestigator Robert L. Byer.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • 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

  • Characteristics of an axisymmetric sudden expansion flow [microform] : progress report, 1 Jul. 1984 - 1 Jul. 1985 / W.H. Stevenson,and H.D. Thompson.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Orbit transfer rocket engine technology program [microform] : enhanced heat transfer combustor technology : subtasks I & II, task C.1 / by R. D. Baily.

    • Text
    • [Washington, D.C. : National Aeronautical Space and Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Laser doppler velocimeter system for subsonic jet mixer nozzle testing at the NASA Lewis Aeroacoustic Propulsion Lab [microform] / Gary G. Podboy ... [et al.].

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

  • An experimental study of a turbulent boundary layer in the trailing edge region of a circulation-control airfoil [microform] / Jeff Brown.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1995]
    • 1995

  • LDV measurements in an annular combustor model [microform] / Dean A. Barron.

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

  • PIV for turbomachinery applications [microform] / Mark P. Wernet.

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

  • Seeding for laser velocimetry in confined supersonic flows with shocks [microform] / J. Lepicovsky and R.J. Bruckner.

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

  • Acoustic and laser doppler anemometer results for confluent, 22-lobed, and unique-lobed mixer exhaust systems for subsonic jet noise reduction [microform] / M. Salikuddin ... [et al.].

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS36058

  • Acoustic and laser doppler anemometer results for confluent and 120-lobed E³ mixer exhaust systems for subsonic jet noise reduction [microform] / M. Salikuddin ... [et al.].

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS36057

  • Dual mode laser velocimeter [microform].

    • Text
    • [Moffett Field, Calif. : NASA Ames Research Center, 1986]
    • 1986

  • The boundary layer on compressor cascade blades [microform] / submitted by Steven Deutsch and William C. Zierke.

    • Text
    • State College, PA : Applied Research Laboratory, The Pennsylvania State University ; [Washington, D.C. : National Aeronautics and Space Administration, 1984]
    • 1984

  • The boundary layer on compressor cascade blades [microform] / submitted by Steven Deutsch and William C. Zierke.

    • Text
    • State College, PA : Applied Research Laboratory, The Pennsylvania State University ; [Washington, D.C. : National Aeronautics and Space Administration, 1986]
    • 1986

  • Molecular velocimetry using stimulated Raman spectroscopy [microform] / Reginald J. Exton and Mervin E. Hillard.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
    • 1984

  • Laser velocimetry in the low-speed wind tunnels at Ames Research Center [microform] / Kenneth L. Orloff, Philip K. Snyder, and Michael S. Reinath.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1984]
    • 1984

  • Multicomponent velocity measurements in a piston-cylinder configuration using laser velocimentry [microform] / Harold J. Schock, ... [et al.].

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1983]
    • 1983

  • A review of internal combustion engine combustion chamber process studies at NASA Lewis Research Center [microform] / Harold J. Schock.

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

  • Flow visualization in gaseous flows [microform] / Ronald K. Hanson.

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

  • Study of high-speed combustion flows by laser velocimetry [microform] / H. J. Schaefer.

    • Text
    • Saint-Louis, France : [Insitut Franco-Allemand de Recherches] ; [Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1984]
    • 1984

  • The effect of bypass nozzle exit area on fan aerodynamic performance and noise in a model turbofan simulator / Christopher E. Hughes [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 2013.
    • 2013-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo50531

  • Experimental investigation of shock-cell noise reduction for dual-stream nozzles in simulated flight : comprehensive data report / K. Yamamoto [and four others].

    • Text
    • Cincinnati, Ohio : General Electric Company, Aircraft Engine Business Group, February, 1984.
    • 1984-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo58844

  • Experimental investigation of shock-cell noise reduction for dual-stream nozzles in simulated flight : comprehensive data report / K. Yamamoto [and four others].

    • Text
    • Cincinnati, Ohio : General Electric Company, Aircraft Engine Business Group, February, 1984.
    • 1984-2

  • Seeding for laser velocimetry in confined supersonic flows with shocks / J. Lepicovsky and RJ. Bruckner.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, July 1996.
    • 1996-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo69458

  • Evolution of a planar wake in adverse pressure gradient / David M. Driver, George G. Mateer.

    • Text
    • Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, February 2016.
    • 2016-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo73014

  • 14- by 22-foot subsonic tunnel laser velocimeter upgrade / James F. Meyers [and three others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37522

  • Fluorescence-doped particles for simultaneous temperature and velocity imaging / Paul M. Danehy [and seven others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo39987

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