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  • An experimental study of the flowfield on a semispan rectangular wing with a simulated glaze ice accretion [microform] / Abdollah Khodadoust.

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

  • High frequency flow/structural interaction in dense subsonic fluids [microform] / by Baw-Lin Liu and J.M. O'Farrell.

    • Text
    • [Huntsville, Ala.] : Rockwell Aerospace, Space Systems Division, Huntsville Operations ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Implementation of and measurement with the LIPA technique in a subsonic jet [microform] : final report / R.E. Falco.

    • Text
    • East Lansing, MI : Michigan State University, Dept. of Mechanical Engineering ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Shear flow control of cold and heated rectangular jets by mechanical tabs [microform] / W.H. Brown and K.K. Ahuja.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Determination of the pressure drag of airfoils by integration of surface pressures [microform] / Williams H. Phillips.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • Axis switching and spreading of an asymmetric jet [microform] : role of vorticity dynamics / K.B.M.Q. Zaman.

    • 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

  • High frequency flow/structural interaction in dense subsonic fluids [microform] / B.-L. Liu and J.M. O'Farrell.

    • Text
    • Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Wing pressure distributions from subsonic tests of a high-wing transport model [microform] / Zachary T. Applin and Carl L. Gentry, Jr., M.A. Takallu.

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

  • Measurement of gust response on a turbine cascade [microform] : / A.P. Kurkov and B.L. Lucci.

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

  • Spurious frequencies as a result of numerical boundary treatments [microform] / Saul Abarbanel, David Gottlieb.

    • Text
    • Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • Flow in out-of-plane double s-bends [microform] / by M.C. Schmidt, J.H. Whitelaw and M. Yianneskis.

    • Text
    • London, England : Imperial College of Science and Technology, Fluids Section, Mechanical Enginering Dept. : [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Viscous flow computations for elliptical two-duct version of the SSME hot gas manifold [microform] : interim report / by R.P. Roger.

    • Text
    • [Huntsville?], AL : National Aeronautics and Space Administration, Marshall Space Flight Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Hot-wire calibration in subsonic/transonic flow regimes [microform] : summary of research for the period November 18, 1993 through November 17, 1994 / K.A. Nagabushana and Robert L. Ash, principal investigatior.

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

  • TranAir, a full-potential, solution-adaptive, rectangular grid code for predicting subsonic, transonic, and supersonic flows about arbitrary configurations [microform] : user's manual / F.T. Johnson ... [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], 1992.
    • 1992

  • Response of multi-panel assembly to noise from a jet in forward motion [microform] / A. Bayliss ... [et al.].

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • TranAir, a full-potential, solution-adaptive, rectangular grid code for predicting subsonic, transonic, and supersonic flows about arbitrary configurations [microform] : theory document / F.T. Johnson ... [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], 1992.
    • 1992

  • The role of freestream turbulence scale in subsonic flow separation [microform] : interim progress report 2 ... 1 January 1985 - 30 June 1985 / J. Leith Potter ... [et al.].

    • Text
    • Nashville, TN : Vanderbilt University, School of Engineering, Dept. of Mechanical & Materials Engineering ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Prediction of vortex shedding from circular and noncircular bodies in subsonic flow [microform] / Michael R. Mendenhall and Daniel J. Lesieutre.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space 16
    • 1986

  • Effects of cavity dimensions, boundary layer, and temperature on cavity noise with emphasis on benchmark data to validate computational aerocoustic codes [microform] / K.K. Ahuja and J. Mendoza.

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

  • Analysis of boundary conditions for SSME subsonic internal viscous flow analysis [microform] / by A.J. Baker.

    • Text
    • Knoxville, TN : Computational Mechanics Corporation ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • 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

  • Implementation of a two-equation K-[omega] turbulence model in NPARC [microform] / Dennis A. Yoder and Nicholas J. Georgiadis, Paul D. Orkwis.

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

  • A study to determine methods of improving the subsonic performance of a proposed Personnel Launch System (PLS) concept [microform] / B. Spencer, Jr., C.H. Fox, Jr., and J.K. Huffman.

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

  • 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

  • External boundary conditions for three-dimensional problems of computational aerodynamics [microform] / Semyon V. Tsynkov.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Analytical studies of boundary layer generated aircraft interior noise [microform] / M.S. Howe and P.L. Shah.

    • Text
    • Boston, MA : Boston University, College of Engineering ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Role of boundary conditions in Monte Carlo simulation of MEMS devices [microform] / Robert P. Nance, David B. Hash, H.A. Hassan.

    • Text
    • Washington, D.C. : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • An extended Lagrangian method [microform] / Meng-Sing Liou.

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

  • 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

  • Analysis of Particle Image Velocimetry (PIV) data for application to subsonic jet noise studies [microform] / James L. Blackshire.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Entry dispersion analysis for the Stardust comet sample return capsule [microform] / Prasun N. Desai, Robert A. Mitcheltree, F. McNeil Cheatwood.

    • Text
    • Reston, VA : American Institute of Aeronautics and Astronautics ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Application of the pressure sensitive paint technique to steady and unsteady flow [microform] / Y. Shimbo, R. Mehta, B. Cantwell.

    • Text
    • [Stanford, Calif.?] : Joint Institute for Aeronautics and Acoustics ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • RNS applications for interacting sub- and supersonic flows [microform] : final report, NASA grant no. NAG1-1553, 11/19/93-5/18/97 / Stanley G. Rubin [principal investigator].

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

  • Numerical simulation of jet aerodynamics using the three-dimensional Navier-Stokes code PAB3D [microform] / S. Paul Pao, Khaled S. Abdol-Hamid.

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

  • Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code [microform] / Wendy B. Lessard.

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

  • Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle [microform] / Roger A. Lepsch, Jr. and George M. Ware, Ian O. MacConochie.

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

  • Response of high subsonic jet to nonaxisymmetric disturbances [microform] / A. Bayliss, L. Maestrello.

    • Text
    • Reston, VA : American Institute of Aeronautics and Astronautics ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Application of chimera grid scheme to combustor flowfields at all speeds [microform] / Shaye Yungster, Kuo-Huey Chen.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Computational investigations of noise suppression in subsonic round jets [microform] : final report for NASA grant NAG1-1802 / principal investigator, C. David Pruett.

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

  • Natural rolling responses of a delta wing in transonic and subsonic flows [microform] / Margaret A. Menzies and O. Kandil.

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

  • A comparison of interactional aerodynamics methods for a helicopter in low speed flight [microform] / John D. Berry ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Rayleigh scattering diagnostic for measurement of temperature and velocity in harsh environments [microform] / Richard G. Seasholtz and Lawrence C. Greer III.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998

  • The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel [microform] / Norbert Ulbrich.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • A numerical simulator for three-dimensional flows through vibrating blade rows [microform] / H. Andrew Chuang and Joseph M. Verdon.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Global artificial boundary conditions for computation of external flow problems with propulsive jets [microform] / Semyon Tsynkov ... [et al].

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998

  • Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet [microform] / Michael K. Ponton, Lawrence S. Ukeiley, Sang W. Lee.

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

  • Noise reduction with lobed mixers [microform] : nozzle-length and free-jet speed effects / Vinod G. Mengle ... [et al.].

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, VA : National Technical Information Service, distributor, [1997]
    • 1997

  • Unsteady aerodynamics [microform] : subsonic compressible inviscid case / A.V. Balakrishman.

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

  • Large Engine Technology (LET) task XXXVII low-bypass ratio mixed turbofan engine subsonic jet noise reduction program test report [microform] / Joseph R. Hauser, Steven H. Zysman, and Thomas J. Barber.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001

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