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  • 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

  • Improved nozzle testing techniques in transonic flow, edited by A. Ferri.

    • Text
    • [Neuilly sur Seine, France, 1975]
    • 1975
    • 1 Item
    FormatCall NumberItem Location
    Text VDS (AGARDograph, no. 206) no. 206-208 (1975)Offsite

  • Parametric experimental investigation of a scramjet nozzle at Mach 6 with freon and argon or air used for exhaust simulation [microform] / James M. Cubbage, William J. Monta.

    • Text
    • [Washington, DC] : 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

  • Aeropropulsive characteristics of canted twin pitch-vectoring nozzles at Mach 0.20 to 1.20 [microform] / Francis J. Capone, Mary L. Mason, and George T. Carson, Jr.

    • Text
    • [Washington, DC] : 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

  • Static internal performance of ventral and rear nozzle concepts for short-takeoff and vertical-landing aircraft [microform] / Richard J. Re and George T. Carson, Jr.

    • Text
    • [Washington, DC] : 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

  • Hydraulic model studies : aeration of the submerged jet-flow gates at Seminoe Dam / by K. Warren Frizell.

    • Text
    • Denver, Colo. : Hydraulics Branch, Research and Laboratory Services Division, Denver Office, U.S. Dept. of the Interior, Bureau of Reclamation, [1990]
    • 1990-2

  • Evaluation of water cooled supersonic temperature and pressure probes for application to 2000̊F flows [microform] / Nicholas T. Lagen, John M. Seiner.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
    • 1990

  • Static performance of a cruciform nozzle with multiaxis thrust-vectoring and reverse-thrust capabilities [microform] / David J. Wing and Scott C. Asbury.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1992.
    • 1992

  • Thermal/structural analysis of a transpiration cooled nozzle [microform] / Peyton B. Gregory ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1992]
    • 1992

  • Divergence thrust loss calculations for convergent-divergent nozzles [microform] : extensions to the classical case / Jeffrey J. Berton.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, [1991]
    • 1991

  • Parametric study of afterbody/nozzle drag on twin two-dimensional convergent-divergent nozzles at mach numbers from 0.60 to 1.20 [microform] / Odis C. Pendergraft, Jr., James R. Burley and E. Ann Bare.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va.? : National Technical Information Service [distributor], 1986.
    • 1986

  • Experimental investigation of nozzle/plume aerodynamics at hypersonic speeds [microform] / prepared by Eloret Institute.

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

  • Aircraft ground test and subscale model results of axial thrust loss caused by thrust vectoring using turning vanes [microform] / Steven A. Johnson.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1992.
    • 1992

  • Full Navier-Stokes analysis of a two-dimensional mixer/ejector nozzle for noise suppression [microform] / James R. DeBonis.

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

  • Experimental investigation of the effects of aft blowing with various nozzle exit geometries on a 3.0 caliber tangent Ogive at high angles of attack [microform] : forebody pressure distributions / N.M. Gittner and N. Chokami.

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

  • A nozzle internal performance prediction method [microform] / John R. Carlson.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1992.
    • 1992

  • Experimental research of the aerodynamics of nozzles and plumes at hypersonic speeds [microform] / Earl R. Keener.

    • Text
    • [Moffett Field, Calif.] : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Internal performance of two nozzles utilizing gimbal concepts for thrust vectoring [microform] / Bobby L. Berrier and John G. Taylor.

    • Text
    • [Washington, DC] : 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

  • Static investigation of a two-dimensional convergent-divergent exhaust nozzle with multiaxis thrust-vectoring capability [microform] / John G. Taylor.

    • Text
    • [Washington, DC] : 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

  • Jet engine hot parts IR analysis procedure (J-EIRP) [microform] / Joseph F. Baumeister.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • Viscous computations of cold air/airflow around scramjet nozzle afterbody [microform] / Oktay Baysal and Walter C. Engelund.

    • Text
    • [Washington, DC] : 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

  • Static internal performance of a single expansion ramp nozzle with multiaxis thrust vectoring capability [microform] / Francis J. Capone, Alberto W. Schirmer.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1993.
    • 1993

  • Design and evaluation of single and dual flow thrust vector nozzles with post exit vanes [microform] : semi-annual progress report 6/92 - 12/92 / Thomas W. Carpenter; principal investigator.

    • Text
    • San Luis Obispo, Calif. : California Polytechnic State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Evaluation of dual flow, thrust vector nozzles with exhaust stream impingement [microform] : semi-annual progress report 6/92-12/92, NASA-Ames grant number NAG 2-778 / Thomas W. Carpenter; principal investigator.

    • Text
    • San Luis Obispo, Calif. : California Polytechnic State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Viscous flow simulations of internal store carriage and separation [microform] : final report for the period ended May 15, 1991 / by Oktay Baysal.

    • Text
    • Norfolk, Va. : Dept. of Mechanical Engineering & Mechanics, College of Engineering & Technology, Old Dominion University ; [Washington, D.C. : National Aeronautics and Space Administration, 1991]
    • 1991

  • Free jet feasibility study of a thermal acoustic shield concept for AST/VCE application [microform] : dual stream nozzles / B.A. Janardan, J.F. Brausch, and R.K. Majjigi.

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

  • Supersonic jets from bevelled rectangular nozzles [microform] / Edward J. Rice and Ganesh Raman.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle [microform] / Scott C. Asbury.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1993.
    • 1993

  • Evaluation of dual flow, thrust vector nozzles with exhaust stream impingement [microform] : final technical report 10/90 - 7/91, NASA-Ames grant number NAG 2-778 / Thomas W. Carpenter, principal investigator.

    • Text
    • San Luis Obispo, Calif. : California Polytechnic State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • Effect of 'delta tabs' on mixing and axis switching in jets from asymmetric nozzles [microform] / K.B.M.Q. Zaman.

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

  • Alternate nozzle ablative materials program [microform] : final report covering period October 11, 1982 to May 21, 1983 / N.A. Kimmel ; prepared for NASA Marshall Space Flight Center through an agreement with National Aeronautics and Space Administration by Jet Propulsion Laboratory.

    • Text
    • Pasadena, Calif. : The Laboratory ; [Springfield, Va. : National Technical Information Service, 1984]
    • 1984

  • Evaluation of flip-flop jet nozzles for use as practical excitation devices [microform] / Ganesh Raman, Edward J. Rice and David M. Cornelius.

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

  • Mixing and noise benefit versus thrust penalty in supersonic jets using impingement tones [microform] / Ganesh Raman and Edward J. Rice.

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

  • 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

  • Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes [microform] / Robert J. Foley, Odis C. Pendergraft, Jr.

    • 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

  • Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60⁰ [microform] / Laurence D. Leavitt.

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

  • Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles [microform] / Mary L. Mason and Bobby L. Berrier.

    • 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

  • Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20 [microform] / George T. Carson, Jr., and Milton Lamb.

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

  • Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability [microform] / Mary L. Mason and James R. Burley II.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986.
    • 1986

  • Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap [microform] / Richard J. Re and Laurence D. Leavitt.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986.
    • 1986

  • Performance characteristics of an isolated coannular plug nozzle at transonic speeds [microform] / Charles E. Mercer and James R. Burley, II.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, VA : Available from the National Technical Information Service, 1985]
    • 1985

  • Operating characteristics of the multiple critical venturi system and secondary calibration nozzles used for weight-flow measurements in the Langley 16-foot transonic tunnel [microform] / Bobby L. Berrier, Laurence D. Leavitt, and Linda S. Bangert.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
    • 1985
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS96291

  • Effect of jet exit vanes on flow pulsations in an open-jet wind tunnel [microform] / William L. Sellers, III, ... [et al.].

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

  • Flow visualization and interpretation of visualization data for deflected thrust V/STOL nozzles [microform] / H.C. Kao, P. L. Burstadt, and A. L. Johns.

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

  • Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversers / Robert S. Green, George T. Carson, Jr.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
    • 1987
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS112156

  • Flow-field surveys for rectangular nozzles / K. B. M. Q. Zaman.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo28432

  • Numerical method for predicting flow characteristics and performance of nonaxisymmetric nozzles. Part 2-applications / P.D. Thomas ; prepared for Langley Research Center.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo65098

  • Increased jet noise due to a "nominally laminar" state of nozzle exit boundary layer / K.B.M.Q. Zaman.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo81483

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