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Parallel implementation of the discontinuous Galerkin method [microform] / Abdelkader Baggag, Harold Atkins, David Keyes
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
1999
0 resources
Factorizable schemes for the equations of fluid flow [microform] / David Sidilkover.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
1999
0 resources
Unstructured grid Euler method assessment for longitudinal and lateral/directional stability analysis of the HSR Reference H configuration at transonic speeds [microform] / Farhad Ghaffari.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
1999
0 resources
Flutter and forced response analyses of cascades using a two-dimensional linearized Euler solver [microform] / T.S.R. Reddy and R. Srivastava, O. Mehmed.
Microform
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : Available from National Technical Information Service, [1999]
1999
0 resources
Unstructured grid Euler method assessment for longitudinal and lateral/directional aerodynamic performance analysis of the HSR technology concept airplane at supersonic cruise speeds [microform] / Farhad Ghaffari.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information ; Springfield, VA : National Technical Information Service, [distributor, 1999]
1999
0 resources
Implicit schemes and parallel computing in unstructured grid CFD / V. Venkatakrishnan.
Microform
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
The analysis and construction of perfectly matched layers for linearized Euler equations [microform] / J.S. Hesthaven.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, [distributor, 1997]
1997
0 resources
Progress in multi-dimensional upwind differencing [microform] / Bram van Leer.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
1992
0 resources
Development of an aeroelastic code based on an Euler/Navier-Stokes aerodynamic solver [microform] / Milind A. Bakhle ... [et al.].
Microform
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Final report of investigation of source location determination from Magsat magnetic anomalies [microform] : The Euler method approach (NCC 5-70) / prepared by Dhananjay Ravat.
Microform
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Some approaches towards constructing optimally efficient multigrid solvers for the inviscid flow equations [microform] / David Sidilkover.
Microform
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
User's manual for DuctE3D [microform] : a program for 3D Euler unsteady aerodynamic and aeroelastic analysis of ducted fans / R. Srivastava and T.S.R. Reddy.
Microform
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Variational methods in sensitivity analysis and optimization for aerodynamic applications [microform] : progress report for the period ended June 30, 1996 ... under research grant NCC1-68 / by A.H. Ibrahim, G.J.-W. Hou, and S.N. Tiwari, principal investigator ; submitted by the Old Dominion University Research Foundation.
Microform
Norfolk , Va. : Dept. of Mechanical Engineering, College of Engineering & Technology, Old Dominion University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows [microform] : under contract NAS3-26618 / Matthew D. Montgomery and Joseph M. Verdon.
Microform
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1997.
1997
0 resources
Optimum transonic airfoils based on the Euler equations [microform] / Angelo Iollo, Manuel D. Salas.
Microform
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Wing-body aeroelasticity on parallel computers [microform] / Chansup Byun and Guru P. Guruswamy.
Microform
Washington, DC : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Solution-adaptive Cartesian cell approach for viscous and inviscid flows [microform] / William J. Coirier and Kenneth G. Powell.
Microform
Washington, DC : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Numerical study of interaction of a vortical density inhomogeneity with shock and expansion waves [microform] / A. Povitsky, D. Ofengeim.
Microform
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
Eigenmode analysis of boundary conditions for the one-dimensional preconditioned Euler equations [microfiche] / David L. Darmofal.
Microform
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
The space-time conservation element and solution element method--a new high-resolution and genuinely multidimensional paradigm for solving conservation laws. II, Numerical simulation of shock waves and contact discontinuities [microform] / Xiao-Yen Wang, Chuen-Yen Chow, Sin-Chung Chang.
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Euler technology assessment for preliminary aircraft design [microform] : unstructured/structured grid NASTD application for aerodynamic analysis of an advanced fighter/tailless configuration / Todd R. Michal.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : Available from the National Technical Information Service, [1998]
1998
0 resources
Development of a linearized unsteady Euler analysis with application to wake/blade-row interactions [microform] / Joseph M. Verdon, Matthew D. Montgomery, and H. Andrew Chuang.
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
1999
0 resources
Connection between the lattice Boltzmann equation and the beam scheme [microform] / Kun Xu, Li-Shi Luo.
Microform
Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
1999
0 resources
Entropy analysis of kinetic flux vector splitting schemes for the compressible Euler equations [microform] / Lui Shiuhong, Kun Xu.
Microform
Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
1999
0 resources
Perfectly matched layer for linearized Euler equations in open and ducted domains [microform] / C.K.W. Tam and L. Auriault, F. Cambuli.
Microform
Reston, Va. : American Institute of Aeronautics and Astronautics ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Tetrahedral finite-volume solutions to the Navier-Stokes equations on complex configurations [microform] / Neal T. Frink and Shahyar Z. Pirzadeh.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
An automated code generator for three-dimensional acoustic wave propagation with geometrically complex solid wall boundaries [microform] / Rodger William Dyson.
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
1999
0 resources
Assessment of an Euler-interacting boundary layer method using high Reynolds number transonic transport flight data [microform] / Daryl L. Bonhaus and Dal V. Maddalon.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
1998
0 resources
Technique for a very high order nonlinear simulation and validation [microform] / Rodger W. Dyson.
Microform
[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
Flow prediction for propfan engine installation effects on transport aircraft at transonic speeds [microform] / S. S. Samant and N. J. Yu.
Microform
[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
Three-dimensional Euler time accurate simulations of fan rotor-stator interactions [microform] / A.A Boretti.
Microform
[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, 1990]
1990
1 resource
Available online
Euler flow predictions for an oscillating cascade using a high resolution wave-split scheme [microform] / Dennis L. Huff, Timothy W. Swafford, and T.S.R. Reddy.
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
1991
1 resource
Available online
Euler and Navier-Stokes computations for two-dimensional geometries using unstructured meshes [microform] / D.J. Mavriplis.
Microform
Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
1990
1 resource
Available online
Investigation 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.
Microform
[Washington, D.C.] : National Aeronautics and Space Administration, [1990]
1990
1 resource
Available online
Adaptive grid embedding for the two-dimensional flux-split Euler equations [microform] / by Gary Patrick Warren.
Microform
Mississippi State, Miss. : Mississippi State University, Dept. of Aerospace Engineering, [1990]
1990
1 resource
Available online
Stable boundary conditions for Cartesian grid calculations [microform] / M. J. Berger, R. J. LeVeque.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
1990
1 resource
Available online
An efficient method for solving the steady Euler equations [microform] / Meng-Sing Liou.
Microform
[Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
1986
1 resource
Available online
Three-dimensional unsteady Euler euqation solutions using flux vector splitting [microform] / David L. Whitfield.
Microform
Mississippi State, MS : Mississippi State University, Dept. of Aerospace Engineering ; [Hampton, Va. : NASA Langley Research Center, 1983]
1983
0 resources
Eigenmode analysis of unsteady one-dimensional Euler equations [microform] / Michael Giles.
Microform
Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, [1983]
1983
0 resources
High resolution schemes and the entropy condition [microform] / Stanley Osher and Sukumar Chakravarthy.
Microform
Hampton, Va : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, [1983]
1983
0 resources
Spectral methods for the Euler equations [microform] : Fourier methods and shock-capturing / M. Y. Hussaini ... [et al.].
Microform
Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, [1984]
1984
0 resources
Nonlinear acoustic wave propagation in atmosphere [microform] : final report, October 1, 1984 through October 31, 1985 / S.I. Hariharan.
Microform
Tullahoma, TN : The University of Tennessee Space Institute ; [Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1985]
1985
0 resources
Flow instabilities in transonic small disturbance theory [microform] / Marc H. Williams, Samuel R. Bland, and John W. Edwards.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
1985
0 resources
An analysis of rotor blade twist variables associated with different Euler sequences and pretwist treatments [microform] / Kathy Alkire.
Microform
Moffet Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1984]
1984
0 resources
Embedding methods for the steady Euler equations [microform] / Shih-Hung Chang and Gary M. Johnson.
Microform
[Washington, D.C. : National Aeronautics and Space Administration, 1983]
1983
0 resources
Euler solutions using an implicit multigrid technique [microform] / Chien-peng Li.
Microform
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
1986
0 resources
A simulation of rotor-stator interaction using the Euler equations and patched grids [microform] / Man Mohan Rai.
Microform
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.
Microform
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
1985
0 resources
A genuinely multi-dimensional upwind cell-vertex scheme for the Euler equations [microform] / Kenneth G. Powell and Bram van Leer.
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Institute for Computational Mechanics in Propulsion, [1989]
1989
1 resource
Available online
High speed corner and gap seal computations using an LU-SGS scheme [microform] / William J. Coirier.
Microform
[Washington, D.C.] : National Aeronautics and Space Administration, [1989]
1989
1 resource