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Factorizable schemes for the equations of fluid flow [microform] / David Sidilkover.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
1999
0 resources
A flux splitting scheme with high-resolution and robustness for discontinuities [microform] / Yasuhiro Wada, Meng-Sing Liou.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
A phase equation approach to boundary layer instability theory [microform] : Tollmien Schlichting waves / Philip Hall.
Text
Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
A new Reynolds stress algebraic equation model [microform] / Tsan-Hsing Shih and Jiang Zhu, John L. Lumley.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Control theory based airfoil design using the Euler equations [microform] / Antony Jameson and James Reuther.
Text
[Moffett Field, Calif.] : Research Institute for Advanced Computer Science, NASA Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
An asymptotic induced numerical method for the convection-diffusion-reaction equation [microform] / Jeffrey S. Scroggs, Danny C. Sorensen.
Text
Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
1988
0 resources
On the breakup of viscous liquid threads [microform] / Demetrios T. Papagerogiou.
Text
Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Modeling of nonequilibrium space plasma flows [microform] / Tamas Gombosi.
Text
Ann Arbor, Mich. : The University of Michigan, Dept. of Atmospheric, Oceanic, and Space Science, Space Physics Research Laboratory ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Computation of asymmetric supersonic flows around cones at large incidence [microform] : final report / principal investigator, David Degani.
Text
Technion City, Haifa, Israel : Technion Research & Development Foundation ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987?]
1987
0 resources
Application of Navier-Stokes code PAB3D with k-e turbulence model to attached and separated flows [microform] / Khaled S. Abdol-Hamid, B. Lakshmanan, John R. Carlson.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Development of direct-inverse 3-D method for applied aerodynamic design and analysis [microform] : semiannual progress report, July 1, 1986 - December 31, 1986 / Leland A. Carlson.
Text
College Station, Tex. : Texas Engineering Experiment Station, Aerospace Engineering Department, Texas A&M University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
1987
0 resources
A comparison of experimental and theoretical results for labyrinth gas seals [microform] / by Joseph Kirk Scharrer.
Text
College Station, Tex. : Texas A&M University, Turbomachinery Laboratories, Mechanical Engineering Dept. : [Washington, DC : National Aeronautics and Space Administration : Springfield, Va. : National Technical Information Service, distributor, 1987]
1987
0 resources
Semi-implicit and fully implicit shock-capturing methods for hyperbolic conservation laws with stiff source terms [microform] / H.C. Yee, Judy L. Shinn.
Text
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1986]
1986
0 resources
Third-moment closure of turbulence for predictions of separating and reattaching shear flows [microform] : final report on "A study of Reynolds-Stress Closure Model" / by R.S. Amano, principal investigator and Pankaj Goel, research assistant.
Text
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
1986
0 resources
Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows [microform] / by Scott T. Imlay.
Text
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service, 1986.
1986
0 resources
Robust integration schemes for generalized viscoplasticity with internal-state variables. Part I, Theoretical developments and applications [microform] / Atef F. Saleeb and Wei Li.
Text
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Robust integration schemes for generalized viscoplasticity with internal-state variables. Part II, Algorithmic developments and implementation [microform] / Wei Li, Atef F. Saleeb.
Text
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Transition and mixing in axisymmetric jets and vortex rings [microform] / Gary A. Allen, Jr., and Brian J. Cantwell.
Text
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1986.
1986
0 resources
Final report on adaptive computational methods for SSME internal flow analysis [microform] / by J. Tinsley Oden.
Text
[Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
1986
0 resources
Breakdown of the conservative potential equation [microform] / M.D. Salas and Clyde R. Gumbert.
Text
[Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : National Technical Information Service, distributor], 1986.
1986
0 resources
Thermodynamic evaluation of transonic compressor rotors using the finite volume approach [microform] : status report, August 1986 on NASA grant no. NAG 3-593 / by Stephen Nicholson, John Moore.
Text
Blacksburg, Va. : Mechanical Engineering Dept., Virginia Polytechnic Institute and State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
1986
0 resources
Application of the space-time conservation element and solution element method to two-dimensional advection-diffusion problems [microform] / Xiao-Yen Wang and Chuen-Yen Chow, Sin-Chung Chang.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
The method of space-time conservation element and solution element [microform] : development of a new implicit solver / S.C. Chang ... [et al.].
Text
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
3-D unstructured method for flows past bodies in 6-DOF relative motion [microform] : preprint from proceedings of 6th International Symposium of Computational Fluid Dynamics, Japan Society of Computational Fluid Dynamics, September 4-8, 1995, Lake Tahoe, Nevada / K.P. Singh and Oktay Baysal.
Text
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995?]
1995
0 resources
Termination shock response to large-scale solar wind fluctuations [microform] / R.S. Steinolfson.
Text
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Comparison of several dissipation algorithms for central difference schemes [microform] / R.C. Swanson, R. Radespiel, E. Turkel.
Text
Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Multi-dimensional asymptotically stable finite difference schemes for the advection-diffusion equation [microform] / Saul Abarbanel, Adi Ditkowski.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method [microform] / John W. Edwards.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Efficient gradient-based shape optimization methodology using inviscid/viscous CFD [microform] : summary of research report for the period of March 9, 1995 to March 8, 1997, grant# NCC-1-211 / by Oktay Baysal, principal investigator ; submitted by the Old Dominion University Research Foundation.
Text
Norfolk, Va. : Dept. of Aerospace Engineering, College of Engineering and Technology, Old Dominion University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
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
0 resources
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
0 resources
Unsteady, transonic flow around delta wings undergoing coupled and natural modes response : a multidisciplinary problem / by Margaret Anne Menzies ; a dissertation submitted to the Faculty of Old Dominion University in partial fulfillment of the requirement for the degree of Doctor of Philosophy, Aerospace Engineering, Old Dominion University.
Text
[Norfolk, VA : Old Dominion University ; Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Aerodynamic design on unstructured grids for turbulent flows [microform] / W. Kyle Anderson and Daryl L. Bonhaus.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
A gas-kinetic scheme for reactive flows [microform] / Youg-Sheng Lian, Kun Xu.
Text
Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
1998
0 resources
Three-dimensional simulations of Marangoni-Benard convection in small containers by the least-squares finite element method [microform] / Sheng-Tao Yu ... [et al.].
Text
Washington, D.C. : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Deterministic stress modeling of hot gas segregation in a turbine [microform] / Judy Busby ... [et al.].
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Study of two-dimensional compressible non-acoustic modeling of stirling machine type components [microform] / Roy C. Tew, Jr., Mounir B. Ibrahim.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information, [2001]
2001
1 resource
Available online
Adobe Acrobat Reader requiredThe P¹-RKDG method for two-dimensional Euler equations of gas dynamics [microform] / Bernardo Cockburn, Chi-Wang Shu.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center : ICASE, [1991]
1991
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS67047Investigation of advanced counterrotation blade configuration concepts for high speed turboprop systems. Task 1, Ducted propfan analysis [microform] : final report / Edward J. Hall, Robert A. Delaney, and James L. Bettner.
Text
[Washington, D.C.] : National Aeronautics and Space Administration, [1990]
1990
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS67939A model for closing the inviscid form of the average-passage equation system [microform] / John J. Adamczyk, and Richard A. Mulac and Mark L. Celestina.
Text
[Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
1986
0 resources
Three-dimensional unsteady Euler euqation solutions using flux vector splitting [microform] / David L. Whitfield.
Text
Mississippi State, MS : Mississippi State University, Dept. of Aerospace Engineering ; [Hampton, Va. : NASA Langley Research Center, 1983]
1983
0 resources
Numerical approach for the aerodynamic analysis of airfoils with laminar separation [microform] / prepared by David W. Halt and Dean R. Bristow.
Text
St. Louis, Mo. : McDonnel Douglas Corporation, McDonnel Aircraft Company ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
1985
0 resources
Newton like [microform] : minimal residual methods applied to transonic flow calculations / Yau Shu Wong.
Text
Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, [1984]
1984
0 resources
Entropy condtion satisfying approximations for the full potential equations of transonic flow [microform] / Stanley Osher, Woodrow Whitlow, Jr., and Mohamed Hafez.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
1984
0 resources
The movement of water droplets in clouds around the nose of an atmospheric research aircraft [microform] / P. Feuillebois, M.F. Scibilia.
Text
Washington, D.C. : National Aeronautics and Space Administration, [1983]
1983
0 resources
Aerodynamic effect of combustor inlet-air pressure on fuel jet atomization [microform] / Robert D. Ingebo.
Text
[Washington, D.C. : National Aeronautics and Space Administration, 1984]
1984
0 resources
An implicit finite-difference code for a two-equatuion turbulence model for three-dimensional flows [microform] / Upender K. Kaul.
Text
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1985]
1985
0 resources
An implicit, conservative, zonal-boundary scheme for Euler equation calculations [microform] / Man Mohan Rai.
Text
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
1985
0 resources
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/LPS108153The 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/LPS108153No results found from Digital Research Books Beta
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