Research Catalog

  • Teoria si calculul injectoarelor mecanice cu cameră de turbionare.

    • Text
    • [Bucuresti], Editura Academiei Republicii Socialiste România, 1971.
    • 1971
    • 1 Item
    FormatCall NumberItem Location
    Text JSE 73-1543Offsite
  • Fuel-oil injection into blast furnaces : a literature review / [by] H. G. Lunn, G. W. Waterhouse.

    • Text
    • London : Marketing Department, BP Trading, 1975.
    • 1975
    • 1 Item
    FormatCall NumberItem Location
    Text JSG 78-61Offsite
  • Locomotive boiler-feeding devices, by J. W. Harding and G. V. Williamson.

    • Text
    • Scranton, Pa., International textbook company [1935]
    • 1935
    • 1 Item
    FormatCall NumberItem Location
    Text TPE (Harding, J. W. Locomotive boiler-feeding devices)Offsite
  • Locomotive injectors and boiler attachments. Injector department, 1920 edition.

    • Text
    • Philadelphia, Pa., W. Sellers & co., incorporated [c1920]
    • 1920
    • 1 Item
    FormatCall NumberItem Location
    Text TPE (Sellers, William, & co. Locomotive injectors and boiler attachments)Offsite
  • Steam injectors: their theory and use. Tr. from the French of M. Leon Pochet.

    • Text
    • New York, D. Van Nostrand company, 1877.
    • 1877
    • 1 Item
    FormatCall NumberItem Location
    Text VFK (Pochet, L. Steam injectors)Offsite
  • Practice and theory of the injector. By Strickland L. Kneass.

    • Text
    • New York, Wiley, 1894.
    • 1894
    • 1 Item

    Available Online

    http://babel.hathitrust.org/cgi/pt?id=nyp.33433066425632
    FormatCall NumberItem Location
    Text 3-VFH (Kneass, S. L. Practice and theory of the injector. 1894)Offsite
  • Practice and theory of the injector. By Strickland L. Kneass.

    • Text
    • New York, Wiley, 1910.
    • 1910
    • 1 Item
    FormatCall NumberItem Location
    Text VFH (Kneass, S. L. Practice and theory of the injector. 1910)Offsite
  • Injectors; their theory, construction & working.

    • Text
    • Manchester, Eng., Technical pub. co., 1906.
    • 1906
    • 1 Item

    Available Online

    http://babel.hathitrust.org/cgi/pt?id=nyp.33433066421896
    FormatCall NumberItem Location
    Text VFH (Pullen, W. W. F. Injectors)Offsite
  • Thermodynamique du moteur polycarburant à injection / par J. Jalbert, ...

    • Text
    • Paris : J. et R. Sennac, 1945.
    • 1945
    • 1 Item
    FormatCall NumberItem Location
    Text VBA p.v. 1217 no. 1-7Schwarzman Building - General Research Room 315

    Available - Can be used on site. Please visit New York Public Library - Schwarzman Building to submit a request in person.

  • Untersuchungen an Brennstoff-Einspritzsystemen nach dem Akkumulierverfahren, von Dr. Werner Spillman ...

    • Text
    • Zürich, Gebr. Leemann & Co. [1946]
    • 1946
  • Effects of jet swirl on mixing of a light gas jet in a supersonic airstream [microform] / Steven E. Doerner and Andrew D. Cutler.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information ; Springfield, VA : National Technical Information Service [distributor, 1999]
    • 1999
  • Flow visualization of a rocket injector spray using gelled propellant simulants [microform] / James M. Green, Douglas C. Ropp, and James Roncace.

    • Text
    • Brook Park, Ohio : Sverdrup Technology Inc., Lewis Research Center Group ; [Cleveland, Ohio] : Lewis Research Center, National Aeronautics and Space Administration, [1991]
    • 1991
  • Space transportation booster engine thrust chamber technology [microform] : final report / prepared by J.A. Schneider.

    • Text
    • Sacramento, Calif. : Aerojet Propulsion Division ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993
  • Heavy hydrocarbon main injector technology program [microform] : final report / H.A. Arbit, L.M. Tuegel, F.E. Dodd.

    • Text
    • Canoga Park, CA : Rocketdyne Division of Rockwell International Corporation ; Huntsville, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991
  • Test results of the RS-44 integrated component evaluator liquid oxygen-hydrogen rocket engine [microform] : final report / by R.F. Sutton and B.W. Lariviere.

    • Text
    • Cleveland, Ohio : NASA-Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993
  • Development of nonintrusive, scatter-independent techniques for measurement of liquid density inside dense sprays [microform] : interim report / Roy Hartfield.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • Flow induced vibrations in the SSME injector heads [microform] : final report no. RI/RD 91-157.

    • Text
    • Canoga Park, CA. : Rockwell International, Rocketdyne Division ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991
  • 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
  • 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
  • Operator, organizational, direct support, and general support maintenance manual including repair parts list for test set, injector (Bacharach Instrument Company) (4910-00-355-6248), model YHQ [microform].

    • Text
    • [Washington, D.C.] : Headquarters, Dept. of the Army, [1995]
    • 1995
  • An experimental study of characteristic combustion-driven flow for CFD validation [microform] : final report for NASA contract NAS8-38862 / by Robert J. Santoro.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997
  • Flow distribution around the SSME main injector assembly using porosity formulation [microform] / Gary C. Cheng, Yen-Sen Chen, and Ten-See Wang.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Development of a device to deploy fluid droplets in microgravity [microform] / David W. Robinson and An-Ti Chai.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997
  • Thruster injector faceplate testing in support of the aerojet Rocket-based combined cycle (RBCC) concept [microform] / M.M. Fazah and J.M. Cramer.

    • Text
    • [Marshall Space Flight Center, Ala.] : National Aeronautics and Space Administration, Marshall Space Flight Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998
  • Analysis and modeling of a two-phase jet pump of a thermal management system for aerospace applications [microform] / S.A. Sherif ... [et al.].

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998
  • Development of tripropellant CFD design code [microform] : contract no.--NAS8-40583 : final report / prepared by Richard C. Farmer, Gary C. Cheng, Peter G. Anderson.

    • Text
    • Huntsville, AL : SECA, Inc. ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998
  • Injector mixing efficiency experiments [microform] : final report : contract number NAS8-38609 D.O. 159 / prepared by Marlow D. Moser, principal investigator.

    • Text
    • [Huntsville, Ala. : University of Alabama in Huntsville], Propulsion Research Center ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998
  • Experimental evaluation of a subscale gaseous hydrogen/gaseous oxygen coaxial rocket injector [microform] / Timothy D. Smith ... [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/LPS43891
  • Space station hydrogen/oxygen thruster technology / G.L. Briley and R.S. Iacabucci.

    • Text
    • [Cleveland, Ohio] : [National Aeronautics and Space Administration, Lewis Research Center], [1988]
    • 1988
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS47226
  • 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
  • Combustion performance and heat transfer characterization of LOX/hydrocarbon type propellants [microform] : final report, volume 2 / prepared by L. Schoenman.

    • Text
    • Sacramento, Calif. : Aerojet Liquid Rocket Company, [1983]
    • 1983
  • 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
  • LOX/hydrogen coaxial injector atomization test program [microform] / M. Zaller.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60988
  • The structural dynamics analysis of the main injector LOX inlet tee and its redesign [microform] / [E. Romano].

    • Text
    • [Canoga Park, Calif. : Rockwell International, Rocketdyne Division? ; Washington, D.C. : National Aeronautics and Space Administration?, 1989?]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69840
  • Low loss injector for space shuttle main engine [microform] : final report / George L. von Pragenau.

    • Text
    • [Marshall Space Flight Center, Ala.] : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1984]
    • 1984
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS99028
  • Current status of superheat spray modeling with NCC / M.S. Raju, Dan L. Bulzan.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo31844
  • Temperature and species measurements of combustion produced by a 9-point lean direct injector / Sarah A. Tedder and Yolanda R. Hicks, Randy J. Locke.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo51522
  • Development of a device to deploy fluid droplets in microgravity / David W. Robinson and An-Ti Chai.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, July 1997.
    • 1997-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo72614
  • A comparative test of steam injectors / by George Henry Trautmann.

    • Text
    • 1897
    • 1 Item
    FormatCall NumberItem Location
    Text VFC p.v. 12 no. 1-17Schwarzman Building - General Research Room 315

    Available - Can be used on site. Please visit New York Public Library - Schwarzman Building to submit a request in person.

  • Experimental evaluation of a subscale gaseous hydrogen/gaseous oxygen coaxial rocket injector / Timothy D. Smith [and four others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, November 2002.
    • 2002-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS43891
  • 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
  • Thruster injector faceplate testing in support of the aerojet rocket-based combined cycle (RBCC) concept / M.M. Fazah and J.M. Cramer.

    • Text
    • Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, May 1998.
    • 1998-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo83111
  • The Hancock Inspirator Co., sole manufacturers of the Hancock inspirator, made in various types for all kinds of duty : the Hancock ejector, the "Loftus" automatic injector, the Hancock "hydro-carbon burner," the Hancock "purge apparatus," the Hancock shaking grates, high grade valves, general jet apparatus.

    • Text
    • [New York?] : [publisher not identified], 1900.
    • 1900
    • 1 Item
    FormatCall NumberItem Location
    Text VFC p.v. 12 no. 1-17Schwarzman Building - General Research Room 315

    Available - Can be used on site. Please visit New York Public Library - Schwarzman Building to submit a request in person.

  • Photographic study of liquid-oxygen boiling and gas injection in the injector of a chugging rocket engine / by E. William Conrad, Ned P. Hannum, and Harry E. Bloomer.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, December 1964.
    • 1964-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo173089
  • Steam injectors : their theory and use / Tr. from the French of M. Leon Pochet.

    • Text
    • New York : D. Van Nostrand company, 1890.
    • 1890
    • 1 Item
    FormatCall NumberItem Location
    Text 621.18 P75Off-site
  • Practice and theory of the injector / By Strickland L. Kneass.

    • Text
    • New York : Wiley, 1910.
    • 1910
    • 1 Item
    FormatCall NumberItem Location
    Text 621.18 K731Off-site
  • Practice and theory of the injector / By Strickland L. Kneass.

    • Text
    • New York : Wiley, 1894.
    • 1894
    • 1 Item
    FormatCall NumberItem Location
    Text 621.18 K73Off-site
  • Untersuchung eines zweistufigen dampfstrahlapparates mit zwischen- und nachkondensator ... Von dipl.-ing. Werner Koch ...

    • Text
    • Borna, Leipzig, Universitätsverlag von Robert Noske, 1930 .
    • 1930
    • 1 Item
    FormatCall NumberItem Location
    Text Engin FilesOff-site
  • Untersuchungen über den Arbeitsvorgang im verstellbaren Injektor System Stumpf ...

    • Text
    • Berlin, Druck: Buchdruckerei W. Deyhle G.m.b.H. [1929?]
    • 1929
    • 1 Item
    FormatCall NumberItem Location
    Text Engin FilesOff-site
  • A comparative test of steam injectors / By George Henry Trautmann.

    • Text
    • Madison, Wis. : The University, 1897.
    • 1897

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