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  • Inlet flow characteristics during rapid maneuvers for an F/A-18A airplane [microform] / William G. Steenken and John G. Williams, Kevin R. Walsh.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • The effects of vortex ingestion on the flow in a diffusing S-DUCT [microform] / B.J. Wendt and B.A. Reichert.

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

  • Installed F/A-18 inlet flow calculations at 30 degrees angle-of-attack, a comparative study [microform] / C. Frederic Smith and Steve D. Podleski.

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

  • Computational methods for HSCT-inlet controls/CFD interdisciplinary research [microform] / Gary L. Cole ... [et al.].

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

  • 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

  • Inlet flow test calibration for a small axial compressor facility. Part I, Design and experimental results [microform] / D.P. Miller and P.S. Prahst.

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

  • A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application [microform] / Kamlesh Kapoor, Bernard H. Anderson, and Robert J. Shaw.

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

  • Turbulence and pressure loss characteristics of the inlet vanes for the 80-by 120-foot wind tunnel [microform] / Michael R. Dudley.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • A computational and experimental investigation of a three-dimensional hypersonic scramjet inlet flow field [microform] / by Scott Douglas Holland.

    • Text
    • Raleligh, NC : North Carolina State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • The effects of inlet turbulence and rotor/stator interactions on the aerodynamics and heat transfer of a large-scale rotating turbine model [microform] : final report / R.P. Dring ... [et al.].

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : National Technical Information Service, distributor], 1987.
    • 1987

  • A preliminary design study of supersonic through-flow fan inlets [microform] / Paul J. Barnhart.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • 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

  • Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code [microform] / Kamlesh Kapoor, Bernhard H. Anderson, and Robert J. Shaw.

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

  • 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

  • Flow visualization studies of VTOL aircraft models during hover in ground effect [microform] / Nikos J. Mourtos ... [et al.].

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

  • Aeropropulsion '87. Session 3, Internal fluid mechanics research [microform].

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • Mach 10 computational study 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. : National Technical Information Service, distributor, 1995]
    • 1995

  • Nozzle diffuser for use with an open test section of a wind tunnel [microform] / inventor, P. Stephen Barna.

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

  • Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10 [microform] / Scott D. Holland.

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

  • Pan Air application to the F-106B [microform] / Farhad Ghaffari.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • 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

  • Inlet flow test calibration for a small axial compressor rig. Part II, CFD compared with experimental results [microform] / D.P. Miller and P.S. Prahst.

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

  • Summary of investigations of engine response to distorted inlet conditions [microform] / Thomas J. Biesiadny ... [et al.].

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1986?]
    • 1986

  • Numerical simulation of supersonic and hypersonic inlet flow fields [microform] : final report / D. Scott McRae.

    • Text
    • Raleigh, N.C. : Mars Mission Research Center, North Carolina State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Numerical simulation of the flow about the F-18 HARV at high angle of attack [microform] / Scott M. Murman.

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

  • Experimental investigation of wing installation effects on a two-dimensional mixer/ejector nozzle for supersonic transport aircraft [microform] / David J. Anderson, Heather H. Lambert, and Masashi Mizukami.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Reduction of Blade-Vortex Interaction (BVI) noise through X-force control [microform] / Fredric H. Schmitz.

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

  • Evaluation of F/A-18A HARV inlet flow analysis with flight data [microform] / C. Frederic Smith ... [et al.].

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

  • Effects of inlet conditions on crossflow jet mixing [microform] / D.S. Liscinsky and B. True, J.D. Holderman.

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

  • 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

  • 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

  • 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

  • An experimental device for generating high frequency perturbations in supersonic wind tunnels [microform] / Kevin J. Melcher and Mounir B. Ibrahim.

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

  • Estimating engine airflow in gas-turbine powered aircraft with clean and distorted inlet flows [microform] / J.G. Williams and W.G. Steenken, A.J. Yuhas.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack [microform] : contract NAS 3-26617 / Andrew J. Yuhas ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor], 1997.
    • 1997

  • 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

  • Development of an experimental data base to validate compressor-face boundary conditions used in unsteady inlet flow computations [microform] : final technical report / Miklos Sajben, Donald D. Freund.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Inlet development for a rocket based combined cycle, single stage to orbit vehicle using computational fluid dynamics [microform] / J.R. DeBonis, C.J. Trefny, and C.J. Steffen, Jr.

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

  • Management of total pressure recovery, distortion and high cycle fatigue in compact air vehicle inlets [microform] / Bernhard H. Anderson, Henry D. Baust, Johan Agrell.

    • 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/LPS36341

  • Validation of WIND for a series of inlet flows [microform] / John W. Slater, John M. Abbott, and Richard H. Cavicchi.

    • 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/LPS46512

  • 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

  • Hot gas ingestion test results of a two-poster vectored thrust concept with flow visualization in the NASA Lewis 9- x 15-foot low speed wind tunnel [microform] / Albert L. Johns, ... [et al.].

    • Text
    • [Cleveland, Ohio : Lewis Research Center, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS62061

  • Computational modeling and validation for hypersonic inlets [microform] / Louis A. Povinelli ; prepared for the 75th Symposium on Hypersonic Combined Cycle Propulsion sponsored by the Propulsion and Energetics Panel of AGARD, Madrid, Spain, May 28-June 1, 1990.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS62529

  • 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

  • Theoretical and experimental study of flow-control devices for inlets of indraft wind tunnels [microform] / James C. Ross.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67453

  • Research on a two-dimensional inlet for a supersonic V/STOL propulsion system [microform] / by J.L. Mark, M.A. McGarry, and P.V. Reagan.

    • Text
    • St. Louis, Mo.] : McDonnell Aircraft Company, McDonnell Douglas Corporation ; [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS71139

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