Research Catalog
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Displaying 1-31 of 31 results
A numerical analysis of heat transfer and effectiveness on film cooled turbine blade tip models [microform] / A.A. Ameri, D.L. Rigby.
- Text
- [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
- 1999
Streamwise vorticity generation in laminar and turbulent jets [microform] / Ayodeji O. Demuren and Robert V. Wilson.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
- 1999
Textbook multigrid efficiency for the incompressible Navier-Stokes equations [microform] : high Reynolds number wakes and boundary layers / James L. Thomas, Boris Diskin, Achi Brandt.
- Text
- Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
- 1999
An experimental and numerical investigation of turbulent vortex breakdown and aircraft wakes [microform] : final report, contract NAG 1-1775 / by Robert E. Spall.
- Text
- [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
- 1996
Laser anemometer measurements of the flow field in a 4:1 pressure ratio centrifugal impeller [microform] / G.J. Skoch ... [et al.].
- Text
- [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
- 1997
An NPARC turbulence module with wall functions [microform] : under cooperative agreement NCC3-370 / J. Zhu and T.-H. Shih.
- Text
- [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
- 1997
The variational method for aerodynamic optimization using the Navier-Stokes equations [microform] : prepared for Langley Research Center under contract NAS1-19480 / Bambang Soemarwoto.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
- 1997
Navier-Stokes computations on full wing-body configuration with oscillating control surfaces [microform] / Shigeru Obayashi, Ing-Tsau Chiu, Guru P. Guruswamy.
- Text
- Washington, DC : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Prediction of heat and mass transfer in a rotating ribbed coolant passage with a 180 degree turn [microform] / David L. Rigby.
- Text
- [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
- 1999
Numerical study of turbulence model predictions for the MD 30P/30N and NHLP-2D three-element highlift configurations [microform] / Joseph H. Morrison.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
- 1998
Noise from supersonic coaxial jets. Part 1, Mean flow predictions [microform] / M.D. Dahl and P.J. Morris.
- Text
- [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
- 1997
Computational aeroheating predictions for X-34 [microform] / William L. Kleb, William A. Wood, and Peter A. Gnoffo.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
- 1998
Reynolds-averaged Navier-Stokes simulations of two partial-span flap wing experiments [microform] / M.A. Takallu, K.R. Laflin.
- Text
- Reston, Va. : American Institute of Aeronautics and Astronautics ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
- 1998
Numerical simulation of complex turbomachinery flows [microform] / A.A. Chernobrovkin and B. Lakshminarayana.
- Text
- [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
- 1999
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
Computational analyses of the LIMX TBCC inlet high-speed flowpath / Vance F. Dippold, III.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
- 2012
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo25003Computational study of the impact of unsteadiness on the aerodynamic performance of a variable-speed power turbine / Gerard E. Welch.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
- 2012
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo27900Ensemble averaged probability density function (APDF) for compressible turbulent reacting flows / Tsan-Hsing Shih, Nan-Suey Liu.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
- 2012
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo32097Aeromechanics analysis of a boundary layer ingesting fan / Milind A. Bakhle [and four others].
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2013.
- 2013
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo51528Development of the Glenn Heat-Transfer (Glenn-HT) computer code to enable Time-Filtered Navier-Stokes (TFNS) simulations and application to film cooling on a flat plate through long cooling tubes / Ali Ameri [and five others].
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2014.
- 2014-4
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo53708Computational simulations of convergent nozzles for the AIAA 1st Propulsion Aerodynamics Workshop / Vance F. Dippold, III.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, August 2014.
- 2014-8
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo57024Performance gains of propellant management devices for liquid hydrogen depots / Jason W. Hartwig, John B. McQuillen and David J. Chato.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2013.
- 2013-2
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo51532Utilizing direct numerical simulations of transition and turbulence in design optimization / Man M. Rai.
- Text
- Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, December 2015.
- 2015-12
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo65165Performance of the widely-used CFD code OVERFLOW on the Pleides supercomputer / Guru P. Guruswamy.
- Text
- Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, May 2017.
- 2017-5
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo81363Using numerical simulations to explore top-mounted propulsion on a conceptual commercial supersonic transport aircraft / David J. Friedlander.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, October 2018.
- 2018-10
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo111267Numerical simulations of a Quiet SuperSonic Technology (QueSST) aircraft preliminary design / David J. Friedlander, Christopher M. Heath, and Raymond S. Castner.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, October 2018.
- 2018-10
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo111274Status of turbulence modeling for hypersonic propulsion flowpaths.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
- 2012
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo29114Large Eddy Simulation of a film cooling flow injected from an inclined discrete cylindrical hole into a crossflow with zero-pressure gradient turbulent boundary layer / Perry L. Johnson, Vikram Shyam.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2012.
- 2012
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo32522An empirical temperature variance source model in heated jets / Abbas Khavaran, James Bridges.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2012.
- 2012
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo37225Modeling and prediction of the noise from non-axisymmetric jets / Stewart J. Leib.
- Text
- Brook Park, Ohio : Ohio Aerospace Institute ; Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, March 2014.
- 2014-3
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo53475Simulations of turbulent momentum and scalar transport in confined swirling coaxial jets / Tsan-Hsing Shih, Nan-Suey Liu.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, August 2014.
- 2014-8
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo56725
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