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Accuracy of schemes for the Euler equations with nonuniform meshes

Turkel, E.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center : Institute for Computer Applications in Science and Engineering, [1985] 1985

Accuracy of schemes with nonuniform meshes for compressible fluid flows

Turkel, E.
Hampton, Va. : Institute for Computer Applications in Science and Engineering, National Aeronautics and Space Administration, Langley Research Center, [1985] 1985

Advances of computational fluid dynamics in nuclear reactor design and safety assessment

Joshi, Jyeshtharaj, author.
Duxford, United Kingdom : Woodhead Publishing, [2019] 2019

Aerodynamic design and computational analysis of a spacecraft cabin ventilation fan

Tweedt, Daniel L. (Daniel Lawrence)
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010] 2010

The aerodynamic design of the oblique flying wing supersonic transport

Van der Velden, Alexander J. M.
Palo Alto, Calif. : Stanford University ; Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1990] 1990

Algebraic turbulence modeling for unstructured and adaptive meshes

Mavriplis, Dimitri.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990] 1990

The analysis and simulation of compressible turbulence

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990] 1990

Analysis of coupled seals, secondary and powerstream flow fields in aircraft and aerospace turbomach

Athavale, M. M.
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2005] 2005

Analysis of internal flows relative to the space shuttle main engine final report.

Huntsville, AL : Lockheed Missiles & Space Company, Inc., Huntsville Engineering Center ; Marshall Space Flight Center, AL : National Aeronautics and Space Administration, [1987] 1987

Application of a Runge-Kutta scheme for high-speed inviscid internal flows

Moitra, Anutosh.
Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center Universities Space Research Association, [1986] 1986

Applications of the Lattice Boltzmann method to complex and turbulent flows

Luo, Li-Shi.
Hampton, Va. : ICASE, NASA Langley Research Center ; Springfield, Va. : For sale by the National Technical Informaton Service, [2002] 2002

Assessment of NASA's aircraft noise prediction capability

Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012] 2012

Balancing power absorption and structural loading for an assymmetric heave waveenergy converter in r

Tom, Nathan M., author.
[Golden, Colo.] : National Renewable Energy Laboratory, 2016. 2016

Blended wing body concept development with open rotor engine intergration

Pitera, David M., author.
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, November 2011. 2011-

CFD simulations for the effect of unsteady wakes on the boundary layer of a highly loaded low-pressu

Vinci, Samuel J., author.
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2012. 2012-

A CFD study of tilt rotor flowfields

Fejtek, Ian.
Stanford, CA : Stanford University, Dept. of Aeronautics and Astronautics : Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center, [1989] 1989

Computational aerodynamic simulations of a spacecraft cabin ventilation fan design

Tweedt, Daniel L. (Daniel Lawrence)
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010] 2010

Computational analyses of propulsion aeroacoustics for mixed flow nozzle pylon installation at takeo

Massey, Steven James.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information, [2001] 2001

Computational analysis of the SSME fuel preburner flow final report

Wang, Ten-See.
Huntsville, AL : Continuum, Inc. ; Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1986] 1986

Computational fluid dynamics

Amsterdam ; Boston : Elsevier, 2006. 2006

Computational fluid dynamics : a practical approach

Tu, Jiyuan, author.
Amsterdam : Butterworth-Heinemann, 2018. 2018

Computational fluid dynamics : a practical approach

Tu, Jiyuan.
Amsterdam ; Boston : Butterworth-Heinemann, 2008. 2008

Computational fluid dynamics : a practical approach

Tu, Jiyuan.
Amsterdam ; Boston : Elsevier/Butterworth-Heinemann, ©2013. 2013

Computational fluid dynamics : a practical approach.

Tu, Jiyuan, author.
Amsterdam : Butterworth-Heinemann, 2023. 2023

Computational fluid dynamics applied to waste-to-energy processes a hands-on approach

Silva, Valter Bruno Reis E.
Oxford : Butterworth-Heinemann, 2020. 2020

Computational fluid dynamics : principles and applications

Blazek, Jiri, author.
Amsterdam ; San Diego : Butterworth Heinemann, [2015] 2015

Computational fluid dynamics : principles and applications

Blazek, J.
Amsterdam ; San Diego : Elsevier, 2005. 2005

Computational fluid mechanics utilizing the variational principle of modeling damping seals

Huntsville, AL : Continuum, Inc., April 10, 1984. 1984-

A computational investigation of gear windage

Hill, Matthew J., author.
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2012. 2012

Computational study of near-limit propagation of detonation in hydrogen-air mixtures

Yungster, Shaye.
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va.: For sale by the National Technical Information Service, 2002] 2002

Computational work to support FAP/SRW variable-speed power-turbine development

Ameri, Ali A., author.
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012] 2012

A critical comparison of turbulence models for homogeneous shear flows in a rotating frame

Speziale, C. G. (Charles G.), 1948-
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989] 1989

Current capabilities and future directions in computational fluid dynamics

National Research Council (U.S.). Committee to Assess Current Capabilities and Future Directions in Computational Fluid Dynamics.
Washington, D.C. : National Academy Press : Available from Aeronautics and Space Engineering Board, National Research Council, 1986. 1986

Development and validation of a multidisciplinary tool for accurate and efficient rotorcraft noise p

Liu, Yi.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011] 2011

Development of a computational aero/fluids analysis system final report

Kelley, P. B.
Huntsville, AL : Lockheed Missiles & Space Company, Inc., Huntsville Engineering Center ; Marshall Space Flight Center, AL : National Aeronautics and Space Administration, [1987]. 1987

Development of detonation modeling capabilities for rocket test facilities: hydrogen-oxygen-nitrogen

Allgood, Daniel C., author.
Stennis Space Center, MS : National Aeronautics and Space Administration, Stennis Space Center, April 2016. 2016-

A dual potential formulation of the Navier-Stokes equations

Gegg, S. G., author.
[Ames, Iowa ] : Heat Transfer Laboratory, Engineering Research Institute, Iowa State University ; Moffett Field, California : NASA-Ames Research Center, [1989?] 1989

Dual-pump CARS development and application to supersonic combustion

Magnotti, Gaetano, author.
Hampton, Va.: National Aeronautics and Space Administration, Langley Research Center, [2012] 2012

Duct flow nonuniformities effects of struts in SSME HGM IIp+s : interim report

Burke, Roger.
Huntsville, AL : Lockheed Missiles & Space Company, Inc., Huntsville Engineering Center ; Marshall Space Flight Center, AL : National Aeronautics and Space Administration, [1988] 1988

Duct flow nonuniformities study for Space Shuttle main engine technical report

Thoenes, Jurgen.
Huntsville. AL : Lockheed, Missiles & Space Company. Inc, Huntsville Engineering Center ; National Aeronautics and Space Administration, Marshall Space Flight Center, [1985] 1985

The effect of wake passing on turbine blade film cooling

Heidmann, James D., author.
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, December 1996. 1996-

Effects of rotation on coolant passage heat transfer

[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; East Hartford, Conn. : Pratt & Whitney ; [Springfield, Va. : National Technical Information Service, distributor], 1991-1993. 1993

Efficient grid generation final report

Gutierrez, Bill.
[Northridge, CA : California State University ; Washington, D.C. : National Aeronautics and Space Administration, 1989] 1989

Enhanced design of turbo-jet LPT by separation control using phased plasma actuators

Corke, Thomas C.
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Administration ; Springfield, VA : National Technical Information Service [distributor, 2003] 2003

Entropic invariants of two-phase flows

Barsky, Eugene, 1974- author.
Waltham, Massachusetts : Elsevier Inc., 2015. 2015

Error estimation and uncertainty propagation in computational fluid mechanics

Zhu, J. Z.
Hampton, Va. : ICASE, NASA Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 2002] 2002

Experimental and computational sonic boom assessment of Lockheed-Martin N+2 low boom models

Cliff, Susan E., author.
Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, January 2015. 2015-

Extension of a three-dimensional viscous wing flow analysis

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990] 1990

Extension of a three-dimensional viscous wing flow analysis user's manual : VISTA 3-D code

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990] 1990

Final report for the shuttle flight experiment on USMP-4 in situ monitoring of crystal growth using

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