Research Catalog

  • Flow quality measurements in an aerodynamic model of NASA Lewis' icing research tunnel [microform] / Victor A. Canacci and Jose C. Gonsalez.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999
  • A comparison of experimental and theoretical results for labyrinth gas seals with honeycomb stators [microform] / by Lawrence Allen Hawkins.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988
  • Thermal and structural tests of René 41 honeycomb integral-tank concept for future space transportation systems [microform] / John L. Shideler ... [et al.].

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va.? : National Technical Information Service, distributor], 1992.
    • 1992
  • A modified VAPEPS method for predicting vibroacoustic response of unreinforced mass loaded honeycomb panels [microform] / Mark E. McNelis ; prepared for the 35th technical meeting of the Institute of Environmental Sciences, Anaheim, California, May 1-5, 1989.

    • Text
    • [Washington, DC] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1989]
    • 1989
  • High capacity demonstration of honecomb panel heat pipes [microform] / H.J. Tanzer.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989
  • High temperature be panel development [microform] / R.Hardesty, M.Jensen, and L.Grant.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Center, distributor, 1989]
    • 1989
  • Ceramic honeycomb structures and the method thereof [microform] / inventors, Salvatore R. Riccitiello, Domenick E. Cagliostro.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987
  • Fiber composite sandwich thermostuctural behavior, computationalsimulation [microform] / C.C. Chamis and R.A. Aiello and P.L.N. Murthy.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986
  • Development of metallic thermal protection systems for the reusable launch vehicle [microform] / Max L. Blosser.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Titanium honeycomb panel testing [microform] / W. Lance Richards, Randolph C. Thompson.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1996.
    • 1996
  • Porous and microporous honeycomb composites as potential boundary-layer bleed materials [microform] / D.O. Davis and B.P. Willis, M. Schoenenberger.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997
  • Acoustic treatment design scaling methods [microform].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999-
    • 1999-present
  • A novel method of testing the shear strength of thick honeycomb composites [microform] / A.J. Hodge and A.T. Nettles.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, VA : For sale by the National Technical Information Service, 1991.
    • 1991
  • An examination of impact damage in glass/phenolic and aluminum honeycomb core composite panels [microform] / A.T. Nettles, D.G. Lance, and A.J. Hodge.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, VA : For sale by the National Technical Information Service], 1990.
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS65683
  • Evaluation of a technique to generate artificially thickened boundary layers in supersonic and hypersonic flows [microform] / A.R. Porro ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1991.
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67809
  • Geometric programming prediction of design trends for OMV protective structures [microform] / R.A. Mog, J.R. Horn.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, VA : For sale by the National Technical Information Service], 1990.
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS68967
  • Determination of flight hardware configuration of energy-absorbing attenuator for proposed space station crew and equipment translation aid cart [microform] / Edwin L. Fasanella ... [et al.].

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1991.
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS70366
  • A damage tolerance comparison of composite hat-stiffened and honeycomb sandwich structure for launch vehicle interstage applications / A.T. Nettles.

    • Text
    • Huntsville, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24323
  • Efficient design and analysis of lightweight reinforced core sandwich and PRSEUS structures / Brett A. Bednarcyk ... [and others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24329
  • Calibration of the NASA Glenn 8- by 6-foot supersonic wind tunnel (1996 and 1997 tests) / E. Allen Arrington.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo27462
  • Advanced radiator concepts utilizing honeycomb panel heat pipes (stainless steel) : interim technical report / G. L. Fleischman, H. J. Tanzer.

    • Text
    • Houston, Tex. : National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, [1985]
    • 1985
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo31693
  • Structural analysis and optimization of a composite fan blade for future aircraft engine / Rula M. Coroneos.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo32080
  • Advanced radiator concepts utilizing honeycomb panel heat pipes (stainless steel) [microform] : interim technical report / G. L. Fleischman, H. J. Tanzer.

    • Text
    • Houston, Tex. : National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, [1985]
    • 1985
  • Buckling testing and analysis of honeycomb sandwich panel arc segments of a full-scale fairing barrel / David E. Myers, Evan J. Pineda [and four others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2013-2014.
    • 2013-2014
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo51535
  • Buckling design and analysis of a payload fairing 1/6th cylindrical arc-segment panel / Daniel N. Kosareo, Stanley T. Oliver, Brett A. Bednarcyk.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2013.
    • 2013-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo52886
  • Nondestructive evaluation (NDE) for inspection of composite sandwich structures / Joseph N. Zalameda and F. Raymond Parker.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, November 2014.
    • 2014-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo58378
  • A fully nonmetallic gas turbine engine enabled by additive manufacturing / Joseph E. Grady [and 18 others].

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo59971
  • Titanium honeycomb panel testing / W. Lance Richards, Randolph C. Thompson.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, October 1996.
    • 1996-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65662
  • Experimental and analytical evaluation of a composite honeycomb deployable energy absorber / Karen E. Jackson [and six others].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo33397
  • Progressive damage analysis of bonded composite joints / Frank A. Leone, Jr., Donato Girolamo, Carlos G. Dávila.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo37682
  • Methods for assessing honeycomb sandwich panel wrinkling failures / Bart F. Zalewski and William B. Dial, Brett A. Bednarcyk.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo37870
  • Composite Crew Module (CCM) permeability characterization / Michael T. Kirsch.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, [2013]
    • 2013
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo41418
  • Von der Faser zum Haus : das Potential von gefalteten Wabenplatten aus Papierwerkstoffen in ihrer architektonischen Anwendung / Stephan Schütz.

    • Text
    • Weimar : Bauhaus-Universitätsverlag, in Jonas Verlag für Kunst und Literatur GmbH, [2017]
    • 2017
    • 1 Item
    FormatCall NumberItem Location
    Text TA455.P37 S38 2017gOff-site
  • Physical properties and fabrication details of experimental honey comb-core sandwich house panels / Housing and Home Finance Agency, Office of the Administrator.

    • Text
    • [Washington, D.C.] : Housing and Home Finance Agency, Office of the Administrator, 1948]
    • 1948
    • 1 Item
    FormatCall NumberItem Location
    Text AA3115 Un344 no.1 etc.Off-site
  • Hanikamu chūbu ākitekuchā tekunorojī bukku / Nihon daigaku Adachi purasu Nakanishi kenkyūshitsu ; Keiō gijuku daigaku Ikaga kenkyūshitsu ; HTA kenkyūkai ; Shinkenchikusha =[editors, HTA Association and Shinkenchiku-sha].

    • Text
    • 2009
    • 1 Item
    FormatCall NumberItem Location
    Text TA660.H66 H36 2009gOff-site
  • Fabrication and test of lightweight honeycomb sandwich structures : final report / James A. Scholl, Muriel L. Koss, and Jack E. Dawson.

    • Text
    • Pasadena, CA : Jet Propulsion Lab., California Inst. of Tech. ; Chula Vista, CA : Rohr Corp., 1969.
    • 1969
    • 1 Item
    FormatCall NumberItem Location
    Text TA492.S25 F33 1969Off-site
  • Devash melakhim.

    • Text
    • 2016
    • 1 Item
    FormatCall NumberItem Location
    Text Heb 43102.463Off-site
  • Numerical and experimental investigation of hollow sphere structures in sandwich panels / Thomas Fiedler.

    • Text
    • Stafa-Zuerich ; Enfield, N.H. : Trans Tech Publications, 2008.
    • 2008
    • 1 Item
    FormatCall NumberItem Location
    Text TA418.9.P6 F54 2008Off-site
  • IUTAM symposium on mechanical properties of cellular materials : proceedings of the IUTAM Symposium on Mechanical Properties of Cellular Materials, held September 17-20, 2007, LMT-Cachan, Cachan, France / Han Zhao, N.A. Fleck, editors.

    • Text
    • [Dordrecht] : Springer, c2009.
    • 2009
    • 1 Item
    FormatCall NumberItem Location
    Text TA418.9.F6 I872 2007Off-site
  • Numerical and experimental investigation of hollow sphere structures in sandwich panels / Thomas Fiedler.

    • Text
    • Stafa-Zuerich ; Enfield, N.H. : Trans Tech Publications, 2008.
    • 2008
    • 1 Item
    FormatCall NumberItem Location
    Text TA418.9.P6 F54 2008Off-site
  • IUTAM symposium on mechanical properties of cellular materials : proceedings of the IUTAM Symposium on Mechanical Properties of Cellular Materials, held September 17-20, 2007, LMT-Cachan, Cachan, France / Han Zhao, N.A. Fleck, editors.

    • Text
    • [Dordrecht] : Springer, ©2009.
    • 2009
    • 1 Item
    FormatCall NumberItem Location
    Text TA418.9.F6 I872 2007Off-site

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