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  • Numerical analysis of the trailblazer inlet flowfield for hypersonic Mach numbers [microform] / C.J. Steffen, Jr. and J.R. DeBonis.

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

  • A design strategy for the use of vortex generators to manage inlet-engine distortion using computational fluid dynamics [microform] / Bernhard H. Anderson and Ralph Levy.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • Final technical report on grant NAG3-1567 entitled Inlet distortion in engines on VSTOL aircraft [microform] / submitted to NASA Lewis Research Center ; principal investigator Choon S. Tan, co-investigator Edward M. Greitzer.

    • Text
    • Cleveland, OH : The Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • NASA Lewis Propulsion Systems Laboratory customer guide manual [microform] / Ronald H. Soeder.

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

  • Evaluation of panel code predictions with experimental results of inlet performance for a 17-inch ducted prop/fan simulator operating at mach 0.2 [microform] / D. R. Boldman ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • Computational analysis in support of the SSTO flowpath test [microform] / Beverly S. Duncan and Charles J. Trefny.

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

  • Three dimensional compressible turbulent flow computations for a diffusing S-duct with/without vortex generators [microform] / by Soo-Yong Cho and Isaac Greber.

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

  • Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attack [microform] / Crawford F. Smith.

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

  • Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6 [microform] / Scott D. Holland.

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

  • Active control of fan noise--feasibility study [microform].

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

  • Collection efficiency and ice accretion calculations for a sphere, a swept MS(1)-317 wing, a swept NACA-0012 wing tip, an axisymmetric inlet, and a Boeing 737-300 inlet [microform] / Colin S. Bidwell and Stanley R. Mohler.

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

  • Performance study for inlet installations [microform] / D.C. Bingaman.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Application of CFD to the analysis and design of high-speed inlets [microform] : final report / by William C. Rose.

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

  • Experimental investigation of inlet-combustor isolators for a dual-mode scramjet at a Mach number of 4 [microform] / Saied Enami ... [et al.].

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

  • Study of compressible flow through a rectangular-to-semiannular transition duct / Jeffry Foster ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1995.
    • 1995

  • Effects of initial conditions on a single jet in crossflow [microform] / D.S. Liscinsky and B. True, J.D. Holdeman.

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

  • Method for extracting forward acoustic wave components from rotating microphone measurements in the inlets of turbofan engines [microform] / D.E. Cicon, T.G. Sofrin.

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

  • An investigation of bleed configurations and their effect on shock wave/boundary layer interactions [microform] : final report / Awatef Hamed, principal investigator.

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

  • Experimental investigation of the inlet deflector configuration variation in the flow field at mach 1.9 [microform] : final report / by Kyu C. Hwang, Surrendra N. Tiwari, and Stanley J. Miley.

    • Text
    • Norfolk, VA : Dept. of Mechanical Engineering, College of Engineering & Technology, Old Dominion University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Multigrid methods for aerodynamic problems in complex geometries [microform] : final report / principal investigator: David A. Caughey.

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

  • Fan noise prediction assessment [microform] / Paul H. Bent.

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

  • 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet [microform] / M. Mizukami and J.D. Saunders.

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

  • PARC3D calculations of the F/A-18A HARV inlet vortex generators [microform] / Steve D. Podleski.

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

  • Collection efficiency and ice accretion calculations for a Boeing 737-300 inlet [microform] / Colin S. Bidwell.

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

  • Development of a low-Reynolds number, nonlinear [kappa-epsilon] model for the reduced Navier-Stokes equations [microform] : a final technical report for NASA-LeRC grant NAG-1781 / David A. Boger, T.R. Govindan, and Henry McDonald.

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

  • Improved NASA-ANOPP noise prediction computer code for advanced subsonic propulsion systems [microform].

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

  • Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach [microform] / W.P. Norby, J.A. Ladd, and A.J. Yuhas.

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

  • Flow through a rectangular-to-semiannular diffusing transition duct [microform] / Jeff Foster ... [et al.].

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

  • IPAC--Inlet Performance Analysis Code [microform] / Paul J. Barnhart.

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

  • A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92 [microform] / Richard J. Re and William K. Abeyounis.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow [microform] / Kenneth J. Baumeister and Kevin L. Kreider.

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

  • Fan noise prediction system development [microform] : source/radiation field coupling and workstation conversion for the acoustic radiation code / H.D. Meyer.

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

  • Improved finite element modeling of the turbofan engine inlet radiation problem [microform] / Indranil Danda Roy and Walter Eversman, H.D. Meyer.

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

  • Finite difference time marching in the frequency domain [microform] : a parabolic formulation for aircraft acoustic nacelle design / Kenneth J. Baumeister and Kevin L. Kreider.

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

  • Comparison of the aeroacoustics of two small-scale supersonic inlets [microform] : final technical report, NASA contract #--NAG 3-1539 / principal investigator, Wing Ng.

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

  • Rocket-based combined cycle engine technology development [microform] : inlet CFD validation and application / J.R. DeBonis and S. Yungster.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, Ohio Aerospace Institute, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Aeronautics and Space Administration, distributor], 1996.
    • 1996

  • Experimental investigation of water droplet impingement on airfoils, finite wings, and an S-duct engine inlet [microform] / Michael Papadakis ... [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/LPS36328

  • Design and development of an F/A-18 inlet distortion rake [microform] : a cost and time saving solution / Andrew J. Yuhas ... [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, 1995]
    • 1995
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60790

  • Mach 10 experimental database of a three-dimensional scramjet inlet flow field [microform] / Scott D. Holland.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, VA : Available from the National Technical Information Service, 1995]
    • 1995
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60779

  • Control of flow separation and mixing by aerodynamic excitation [microform] / Edward J. Rice and John M. Abbott ; prepared for the 17th Congress of the International Council of Aeronautical Sciences sponsored by the American Institute of Aeronautics and Astronautics, Stockholm, Sweden, September 9-14, 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/LPS67478

  • A numerical analysis applied to high angle of attack three-dimensional inlets [microform] / Danny P. Hwang.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
    • 1986

  • SSME fuelside preburner two-dimensional analysis [microform] / Thomas J. Van Overbeke and Russell W. Claus.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
    • 1986

  • Air intakes for a probative missile of rocket ramjet [microform] / G. Laruelle.

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

  • Mach 5 inlet CFD and experimental results / Lois J. Weir, and D. R. Reddy, and George D. Rupp.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1989]
    • 1989
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS107989

  • Mach 5 inlet CFD and experimental results [microform] / Lois J. Weir, and D. R. Reddy, and George D. Rupp.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS107989

  • Acoustic mode measurements in the inlet of a model turbofan using a continuously rotating rake [microform] / Laurence J. Heidelberg and David G. Hall.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration, 1992]
    • 1992

  • Shock position control for mode transition in a turbine based combined cycle engine inlet model / Jeffrey T. Csank and Thomas J. Stueber.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo45744

  • Combined cycle engine large-scale inlet for mode transition experiments : system identification rack hardware design / Randy Thomas and Thomas J. Stueber.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, August 2013.
    • 2013-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo49566

  • Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ° angle of attack / Kevin R. Walsh [and three others].

    • Text
    • Edwards, California. : National Aeronautics and Space Administration, Dryden Flight Research Center, April 1997.
    • 1997-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo66657

  • Finite difference time marching in the frequency domain : a parabolic formulation for aircraft acoustic nacelle design / Kenneth J. Baumeister and Kevin L. Kreider.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, September 1996.
    • 1996-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo68473

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