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  • A k-[epsilson] modeling of near wall turbulence [microform] / Z. Yang and T.H. Shih.

    • Text
    • Cleveland, Ohio : NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
    • 1991

  • A comparison of numerical methods for the Rayleigh equation in unbounded domains [microform] / W.W. Liou, P.J. Morris.

    • Text
    • Cleveland, Ohio : Institute for Computational Mechanics in Propulsion and Center for Modeling of Turbulence and Transition, Lewis Research Center, [1991]
    • 1991

  • Workshop on Computational Turbulence Modeling [microform] : proceedings of a workshop sponsored by the Institute for Computational Mechanics in Propulsion and Center for Modeling of Turbulence and Transition, NASA Lewis Research Center, Cleveland, Ohio, September 15-16, 1993.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.
    • 1994

  • Workshop on Engineering Turbulence Modeling : proceedings of the Workshop on Engineering Turbulence Modeling, Cleveland, Ohio, August 21-22, 1991 / sponsored by the Institute for Computational Mechanics in Propulsion and Center for Modeling of Turbulence and Transition, NASA Lewis Research Center.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
    • 1992

  • Characteristics of 3D turbulent jets in crossflow [microform] / A.O. Demuren.

    • Text
    • [Cleveland, Ohio] : NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • Second order modeling of boundary-free turbulent shear flows [microform] / T.-H. Shih, J.-Y. Chen, and J.L. Limley.

    • Text
    • Cleveland, Ohio : NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • A 2-D oscillating flow analysis in Stirling engine heat exchanges [microform] / Kyung H. Ahn and Mounir B. Ibrahim.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : For sale by the National Technical Information Service, distributor, 1991]
    • 1991

  • The flow induced by the coalescence of two initially stationary drops [microform] / M.R. Nobari and G. Tryggvason.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Convergence acceleration for vector sequences and applications to computational fluid dynamics [microform] / Avram Sidi and Mark L. Celestina.

    • Text
    • Cleveland, Ohio : NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • Modeling of wall-bounded complex flows and free shear flows [microform] / Tsan-Hsing Shih, Jiang Zhu, John L. Lumley.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Effects of artificial viscosity on the accuracy of high-Reynolds-number [kappa-epsilon] turbulence model [microform] / Tawit Chitsomboon.

    • Text
    • Cleveland, Ohio : NASA, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • On the behavior of three-dimensional wave packets in viscously spreading mixing layers [microform] / Thomas F. Balsa.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • On bi-grid local mode analysis of solution techniques for 3-D Euler and Navier-Stokes equations [microform] / S.O. Ibraheem and A.O. Demuren.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • A three-dimensional structured/unstructured hybrid Navier-Stokes method for turbine blade rows [microform] / F.-L. Tsung ... [et al.].

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Parallel Navier-Stokes computations on shared and distributed memory architectures [microform] / M. Ehteshamu Hayder, D.N. Jayasimha, and Sasi Kumar Pillay.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • On the convergence of local approximations to pseudodifferential operators with applications [microform] / Thomas Hagstrom.

    • Text
    • Cleveland, Ohio : Institute for Computational Mechanics in Propulsion, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Nonlinear stability of non-stationary cross-flow vortices in compressible boundary layers [microform] / J.S.B. Gajjar.

    • Text
    • [Cleveland, Ohio] : Institute for Computational Mechanics in Propulsion, NASA Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • An outflow boundary condition for aeroacoustic computations [microform] / M. Ehtesham Hayder, Thomas Hagstrom.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, Ohio Aerospace Institute, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • A fully implicit time accurate method for hypersonic combustion [microform] : application to shock-induced combustion instability / Shaye Yungster and Krishnan Radhakrishnan.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, Ohio Aerospace Institute, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Investigation of convection and pressures treatment with splitting techniques [microform] / Siddharth Thakur, Wei Shyy, Meng-Sing Liou.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • A turbulence model for the NPARC code [microform] / J. Zhu and T.H. Shih.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Industry-Wide Workshop on Computational Turbulence Modeling [microform] : proceedings of a workshop / sponsored by the Institute for Computational Mechanics in Propulsion and Center for Modeling of Turbulence and Transition, Ohio Aerospace Institute, Cleveland, Ohio, October 6-7, 1994.

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

  • Comparison of PDF and moment closure methods in the modeling of turbulent reacting flows [microform] / Andrew T. Norris and Andrew T. Hsu.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • On high-order radiation boundary conditions [microform] / Thomas Hagstrom.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Institute for Computational Mechanics in Propulsion, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • On the nonlinear evolution of a stationary cross-flow vortex in a fully three-dimensional boundary layer flow [microform] / J.S.B. Gajjar.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Computations of viscous flows in complex geometries using multiblock grid systems [microform] / Erlendur Steinthorsson and Ali A. Ameri.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Efficient implementation of minimal polynominal and reduced rank extrapolation methods [microform] / Avram Sidi.

    • Text
    • Cleveland, Ohio : NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990

  • Asymptotic analysis of dissipative waves with applications to their numerical simulation [microform] / Thomas Hagstrom.

    • Text
    • Cleveland, Ohio : NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990

  • Parallel/distributed direct method for solving linear systems [microform] / Avi Lin.

    • Text
    • Cleveland, Ohio : NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990

  • Calculation of 3D turbulent jets in crossflow with a multigrid method and a second-moment closure model [microform] / A.O. Demuren ; prepared for the International Symposium on Engineering Turbulence Modelling and Measurements, sponsored by the Assembly of World Conferences on Experimental Heat Transfer, Fluid Mechanics, and Thermodynamics, Dubrovnik, Yugoslavia, September 24-28, 1990.

    • Text
    • Cleveland,Ohio : NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : For sale by the National Technical Information Service, 1990?]
    • 1990

  • Two-dimensional Euler and Navier Stokes time accurate simulations of fan rotor flows [microform] / A.A. Boretti.

    • Text
    • Cleveland, Ohio : NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990

  • Applications of direct numerical simulation of turbulence in second order closures [microform] / Tsan-Hsing Shih and John L. Lumley.

    • Text
    • Cleveland, Ohio : Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Computational study of flow establishment in a ram accelerator [microform] / S. Yungster, K. Radhakrishnan, M.J. Rabinowitz.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Potential theoretic methods for far field sound radiation calculations [microform] / S.I. Hariharan ... [et al.].

    • Text
    • Cleveland, Ohio : NASA, Lewis Research Center, ICOMP ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • On the application of chimera/unstructured hybrid grids for conjugate heat transfer [microform] / Kai-Hsiung Kao and Meng-Sing Liou.

    • Text
    • Cleveland, Ohio : NASA Lewis Research Center, ICOMP ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • A zonal approach for prediction of jet noise [microform] / S.H. Shih and D.R. Hixon, Reda R. Mankbadi.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • A least-squares finite element method for electromagnetic scattering problems [microform] / Jie Wu and Bo-nan Jiang.

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

  • Simulation of two-fluid flows by the least-squares finite element method using a continuous surface tension model [microform] / Jie Wu, Sheng-Tao Yu, and Bo-nan Jiang.

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

  • 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

  • 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

  • Nonlinear comparison of high-order and optimized finite-difference schemes [microform] / R. Hixon.

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

  • Evaluation of boundary conditions for the gust-cascade problem [microform] / R. Hixon and S.-H. Shih, R.R. Mankbadi.

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

  • The effects of crack surface friction and roughness on crack tip stress fields [microform] / Roberto Ballarini and Michael E. Plesha.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1987]
    • 1987
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS92496

  • A realizable Reynolds stress algebraic equation model [microform] / Tsan-Hsing Shih, Jiang Zhu, and John L. Lumley.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion, [1993]
    • 1993
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS97991

  • Calculation of turbulence-driven secondary motion in ducts with arbitrary cross section / A.O. Demuren.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; Cleveland, Ohio : Lewis Research Center, Institute for Computational Mechanics in Propulsion, [1989]
    • 1989
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS108145

  • The Upper-branch stability of compressible boundary layer flows / J.S.B. Gajjar and J.W. Cole.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; Cleveland, Ohio : Lewis Research Center, Institute for Computational Mechanics in Propulsion, [1989]
    • 1989
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS108153

  • A genuninely multi-dimensional upwind cell-vertex scheme for the Euler equations / Kenneth G. Powell and Bram van Leer.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Institute for Computational Mechanics in Propulsion, [1989]
    • 1989
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS107754

  • On the equivalence of a class of inverse decomposition algorithms for solving systems of linear equations / Nai-kuan Tsao.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion, [1989]
    • 1989
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS107751

  • Calculation of turbulence-driven secondary models in ducts with arbitrary cross section [microform] / A.O. Demuren.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; Cleveland, Ohio : Lewis Research Center, Institute for Computational Mechanics in Propulsion, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS108145

  • The Upper-branch stability of compressible boundary layer flows [microform] / J.S.B. Gajjar and J.W. Cole.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; Cleveland, Ohio : Lewis Research Center, Institute for Computational Mechanics in Propulsion, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS108153

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