Explore: Nozzle Flow
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Source: The Open Library
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Search results from The Open Library
1Two-dimensional converging-diverging rippled nozzles at transonic speeds
By John R. Carlson
“Two-dimensional converging-diverging rippled nozzles at transonic speeds” Metadata:
- Title: ➤ Two-dimensional converging-diverging rippled nozzles at transonic speeds
- Author: John R. Carlson
- Language: English
- Number of Pages: Median: 105
- Publisher: ➤ Langley Research Center - National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1994
- Publish Location: ➤ Hampton - Hampton, Va - [Springfield, Va
“Two-dimensional converging-diverging rippled nozzles at transonic speeds” Subjects and Themes:
- Subjects: ➤ Convergent-divergent nozzles - Discharge coefficient - Drag - Nozzle flow - Nozzle geometry - Nozzles - Ripples - Thrust - Trailing edges - Transonic speed - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: ➤ OL19752932M - OL16487219M - OL15403665M - OL16982124M - OL19753709M - OL18076297M
- Online Computer Library Center (OCLC) ID: 32220800
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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2Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows
By Scott T. Imlay
“Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows” Metadata:
- Title: ➤ Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows
- Author: Scott T. Imlay
- Language: English
- Number of Pages: Median: 180
- Publisher: ➤ Langley Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service
- Publish Date: 1986
- Publish Location: ➤ [Springfield, Va - Hampton, Va - [Washington, D.C.]
“Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows” Subjects and Themes:
- Subjects: ➤ Thrust vector control - Finite volume method - Navier-Stokes equation - Thrust reversal - Nozzle flow - Time marching - Computational fluid dynamics - Flow equations - Airplanes - Nozzle geometry - Nozzles - Convergent-divergent nozzles - Numerical solutions - Navier-Stokes equations - Motors
Edition Identifiers:
- The Open Library ID: OL18083141M - OL15417264M - OL20986195M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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3Nozzle flow with vibrational nonequilibrium
By J. H. Heinbockel
“Nozzle flow with vibrational nonequilibrium” Metadata:
- Title: ➤ Nozzle flow with vibrational nonequilibrium
- Author: J. H. Heinbockel
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - Old Dominion University Research Foundation, Dept. of Mathematics & Statistics, College of Sciences - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, D.C - Norfolk, Va
“Nozzle flow with vibrational nonequilibrium” Subjects and Themes:
- Subjects: ➤ Compressible flow - Computational fluid dynamics - Convergent-divergent nozzles - Navier-Stokes equation - Nonequilibrium flow - Nonequilibrium thermodynamics - Nozzle flow - Vibrational states
Edition Identifiers:
- The Open Library ID: OL17793566M - OL15419739M
- Online Computer Library Center (OCLC) ID: 34729069
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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4Theoretical studies of a molecular beam generator
By J. H. Heinbockel
“Theoretical studies of a molecular beam generator” Metadata:
- Title: ➤ Theoretical studies of a molecular beam generator
- Author: J. H. Heinbockel
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Dept. of Mathematics & Statistics, College of Sciences, Old Dominion University
- Publish Date: 1994
- Publish Location: [Springfield, Va - Norfolk, Va
“Theoretical studies of a molecular beam generator” Subjects and Themes:
- Subjects: ➤ Convergent-divergent nozzles - Gas dynamics - High temperature gases - Mathematical models - Molecular beams - Nitrogen - Nonequilibrium flow - Nozzle flow
Edition Identifiers:
- The Open Library ID: OL15393442M - OL15400261M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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5Validation of the NPARC code for nozzle afterbody flows at transonic speeds
By James R. DeBonis
“Validation of the NPARC code for nozzle afterbody flows at transonic speeds” Metadata:
- Title: ➤ Validation of the NPARC code for nozzle afterbody flows at transonic speeds
- Author: James R. DeBonis
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Validation of the NPARC code for nozzle afterbody flows at transonic speeds” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Applications programs (Computers) - Nozzle flow - Afterbodies - Turbulence models - Program verification (Computers) - Transonic speed
Edition Identifiers:
- The Open Library ID: OL17791907M - OL15414431M
- Online Computer Library Center (OCLC) ID: 34041515
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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6Experimental and analytical studies of flow through a ventral and axial exhaust nozzle system for STOVL aircraft
By Barbara S. Esker
“Experimental and analytical studies of flow through a ventral and axial exhaust nozzle system for STOVL aircraft” Metadata:
- Title: ➤ Experimental and analytical studies of flow through a ventral and axial exhaust nozzle system for STOVL aircraft
- Author: Barbara S. Esker
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1991
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Experimental and analytical studies of flow through a ventral and axial exhaust nozzle system for STOVL aircraft” Subjects and Themes:
- Subjects: ➤ Discharge coefficient - Exhaust nozzles - Nozzle flow - STOVL aircraft - Exhaust systems - Propulsion system performance - Nozzle thrust coefficients
Edition Identifiers:
- The Open Library ID: OL18077140M - OL17683086M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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7A first scramjet study
By George Emmanuel
“A first scramjet study” Metadata:
- Title: A first scramjet study
- Author: George Emmanuel
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1989
- Publish Location: ➤ [Washington, DC - Springfield, Va
“A first scramjet study” Subjects and Themes:
- Subjects: ➤ Temperature effects - Lift - Nozzle flow - Thrust - Hypersonic speed - Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL14972502M - OL17683624M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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8First NASA/Industry High Speed Research Program Nozzle Symposium
By First NASA/Industry High Speed Research Program Nozzle Symposium (1992 Cleveland, Ohio)
“First NASA/Industry High Speed Research Program Nozzle Symposium” Metadata:
- Title: ➤ First NASA/Industry High Speed Research Program Nozzle Symposium
- Author: ➤ First NASA/Industry High Speed Research Program Nozzle Symposium (1992 Cleveland, Ohio)
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - National Technical Information Service [distributor
- Publish Date: 1999
- Publish Location: ➤ [Cleveland, Ohio] - Springfield, VA
“First NASA/Industry High Speed Research Program Nozzle Symposium” Subjects and Themes:
- Subjects: ➤ Nozzles - Nozzle design - Nozzle efficiency - Conferences - Technology assessment - Low noise - Nozzle flow
Edition Identifiers:
- The Open Library ID: OL17702764M - OL17592401M
- Online Computer Library Center (OCLC) ID: 43558291
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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9An evaluation of parameters influencing jet mixing using the WIND Navier-Stokes Code
By Mary Ann Dembowski
“An evaluation of parameters influencing jet mixing using the WIND Navier-Stokes Code” Metadata:
- Title: ➤ An evaluation of parameters influencing jet mixing using the WIND Navier-Stokes Code
- Author: Mary Ann Dembowski
- Language: English
- Publisher: ➤ Available from NASA Center for AeroSpace Information - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2002
- Publish Location: Hanover MD - Cleveland, Ohio
“An evaluation of parameters influencing jet mixing using the WIND Navier-Stokes Code” Subjects and Themes:
- Subjects: ➤ Supersonic nozzles - Nozzle flow - Jet mixing flow - Turbulence models - Turbulent mixing - Application programs (Computers) - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL16055617M - OL17618852M
- Online Computer Library Center (OCLC) ID: 53116371
Access and General Info:
- First Year Published: 2002
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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10Numerical investigations in the backflow region of a vacuum plume
By G. S. Liaw
“Numerical investigations in the backflow region of a vacuum plume” Metadata:
- Title: ➤ Numerical investigations in the backflow region of a vacuum plume
- Author: G. S. Liaw
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Alabama A&M University - National Aeronautics and Space Administration
- Publish Date: 1992 - 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC - Normal, Ala
“Numerical investigations in the backflow region of a vacuum plume” Subjects and Themes:
- Subjects: ➤ Exhaust gases - Boltzmann transport equation - Rocket exhaust - Space vehicles - Rarefied gases - Nozzle flow - Plumes - Plumes (Fluid dynamics) - Axisymmetric flow - Propulsion systems - Low density flow - Computer programs - Finite difference theory - Flow distribution - Monte Carlo method - Gas flow
Edition Identifiers:
- The Open Library ID: OL15419030M - OL15367145M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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11Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds
By Jack Nugent
“Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds” Metadata:
- Title: ➤ Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds
- Author: Jack Nugent
- Language: English
- Number of Pages: Median: 120
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - Ames Research Center - For sale by the National Technical Information Service]
- Publish Date: 1987 - 1988
- Publish Location: ➤ Edwards, Calif - [Springfield, Va - [Washington, DC]
“Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds” Subjects and Themes:
- Subjects: Aerodynamics, Transonic - Afterbodies - Nozzle flow - Reynolds number - Transonic Aerodynamics
Edition Identifiers:
- The Open Library ID: OL14662959M - OL18998718M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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12Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability
By David J. Wing
“Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability” Metadata:
- Title: ➤ Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability
- Author: David J. Wing
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1997
- Publish Location: ➤ Hampton, Va - [Springfield, Va - Washington, D.C
“Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability” Subjects and Themes:
- Subjects: ➤ Static models - Transonic wind tunnels - Thrust vector control - Nozzle flow - Internal flow - Convergent-divergent nozzles - Contours
Edition Identifiers:
- The Open Library ID: OL15504473M - OL21855558M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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13Nozzle flow with vibrational nonequilibrium
By John Gary Landry
“Nozzle flow with vibrational nonequilibrium” Metadata:
- Title: ➤ Nozzle flow with vibrational nonequilibrium
- Author: John Gary Landry
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Nozzle flow with vibrational nonequilibrium” Subjects and Themes:
- Subjects: Convergent-divergent nozzles - Nonequilibrium flow - Nozzle flow
Edition Identifiers:
- The Open Library ID: OL17803927M - OL15425849M
- Online Computer Library Center (OCLC) ID: 35455512
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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14Turbulence modelling of flow fields in thrust chambers
By C. P. Chen
“Turbulence modelling of flow fields in thrust chambers” Metadata:
- Title: ➤ Turbulence modelling of flow fields in thrust chambers
- Author: C. P. Chen
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - Research Institute, the University of Alabama in Huntsville
- Publish Date: 1993
- Publish Location: ➤ [Washington, DC - Springfield, Va - [Huntsville, Ala.]
“Turbulence modelling of flow fields in thrust chambers” Subjects and Themes:
- Subjects: ➤ Compressible boundary layer - Flow distribution - Nozzle flow - Rocket thrust - Space shuttle main engine - Thermochemistry - Thrust chambers - Turbulence effects - Wall flow
Edition Identifiers:
- The Open Library ID: OL17796705M - OL15409296M
- Online Computer Library Center (OCLC) ID: 32748855
Access and General Info:
- First Year Published: 1993
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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15Analysis of internal flow in a ventral nozzle for STOVL aircraft
By C. Frederic Smith
“Analysis of internal flow in a ventral nozzle for STOVL aircraft” Metadata:
- Title: ➤ Analysis of internal flow in a ventral nozzle for STOVL aircraft
- Author: C. Frederic Smith
- Language: English
- Number of Pages: Median: 19
- Publisher: ➤ For sale by the National Technical Information Service - NASA
- Publish Date: 1990
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Analysis of internal flow in a ventral nozzle for STOVL aircraft” Subjects and Themes:
- Subjects: ➤ Airplanes - Short take-off and landing aircraft - Nozzles - Ramjet engines - Numerical analysis - V/STOL aircraft - Propulsion system configurations - Ducted flow - Exhaust flow simulation - Nozzle flow - Internal flow
Edition Identifiers:
- The Open Library ID: OL17630528M - OL16137719M
- Online Computer Library Center (OCLC) ID: 24981019
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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16CFD for hypersonic propulsion
By Louis A. Povinelli
“CFD for hypersonic propulsion” Metadata:
- Title: CFD for hypersonic propulsion
- Author: Louis A. Povinelli
- Language: English
- Publisher: Lewis Research Center
- Publish Date: 1991
- Publish Location: [Cleveland, Ohio
“CFD for hypersonic propulsion” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Viscous flow - Airframes - Hypersonics - Three dimensional flow - Hypersonic flight - Propulsion system configurations - Air breathing engines - Nozzle flow - Flow distribution - Propulsion system performance
Edition Identifiers:
- The Open Library ID: OL17725560M - OL17634717M
- Online Computer Library Center (OCLC) ID: 62207170
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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17[An analysis of gamma ray burst time histories]
By Gerald R. Karr
“[An analysis of gamma ray burst time histories]” Metadata:
- Title: ➤ [An analysis of gamma ray burst time histories]
- Author: Gerald R. Karr
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - University of Alabama in Huntsville - University of Alabama in Huntsville, Summer Faculty Fellowship Research Continuation Program
- Publish Date: 1993 - 1994
- Publish Location: ➤ Huntsville, AL - Springfield, Va - [Washington, DC
“[An analysis of gamma ray burst time histories]” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Gamma ray bursts - Heat flux - Nozzle walls - Nozzle flow - Wall temperature - Film cooling
Edition Identifiers:
- The Open Library ID: OL15403244M - OL14707831M
Access and General Info:
- First Year Published: 1993
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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18High speed nozzles task
By A. Hamed
“High speed nozzles task” Metadata:
- Title: High speed nozzles task
- Author: A. Hamed
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - University of Cincinnati - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Cincinnati, Ohio?] - [Washington, DC
“High speed nozzles task” Subjects and Themes:
- Subjects: ➤ Convergent-divergent nozzles - Exhaust nozzles - Nozzle design - Nozzle flow - Pressure ratio - Supersonic speed - Turbulence models
Edition Identifiers:
- The Open Library ID: OL15418953M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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19Enhancement of mixing in a rectangular jet by mechanical tabs
By W. H. Brown
“Enhancement of mixing in a rectangular jet by mechanical tabs” Metadata:
- Title: ➤ Enhancement of mixing in a rectangular jet by mechanical tabs
- Author: W. H. Brown
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration
- Publish Date: 1990
- Publish Location: [Washington, DC]
“Enhancement of mixing in a rectangular jet by mechanical tabs” Subjects and Themes:
- Subjects: ➤ Fluid jets - Jet mixing flow - Nozzle design - Nozzle flow - Performance tests - Tabs (Control surfaces)
Edition Identifiers:
- The Open Library ID: OL15401825M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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20Shear flow control of cold and heated rectangular jets by mechanical tabs
By W. H. Brown
“Shear flow control of cold and heated rectangular jets by mechanical tabs” Metadata:
- Title: ➤ Shear flow control of cold and heated rectangular jets by mechanical tabs
- Author: W. H. Brown
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1989
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Shear flow control of cold and heated rectangular jets by mechanical tabs” Subjects and Themes:
- Subjects: ➤ Boundary layer flow - Flow measurement - Free jets - Jet flow - Jet mixing flow - Nozzle design - Nozzle flow - Nozzle inserts - Shear flow - Subsonic flow - Supersonic flow - Tabs (Control surfaces)
Edition Identifiers:
- The Open Library ID: OL17002529M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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21Advanced space propulsion system flowfield modeling
By S. D Smith
“Advanced space propulsion system flowfield modeling” Metadata:
- Title: ➤ Advanced space propulsion system flowfield modeling
- Author: S. D Smith
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Advanced space propulsion system flowfield modeling” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Inviscid flow - Computerized simulation - Mathematical models - Boundary layer flow - Flow distribution - Nozzle flow - Plumes - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL15544943M
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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22Three-dimensional Navier-Stokes analysis and redesign of an imbedded bellmouth nozzle in a turbine cascade inlet section
“Three-dimensional Navier-Stokes analysis and redesign of an imbedded bellmouth nozzle in a turbine cascade inlet section” Metadata:
- Title: ➤ Three-dimensional Navier-Stokes analysis and redesign of an imbedded bellmouth nozzle in a turbine cascade inlet section
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Three-dimensional Navier-Stokes analysis and redesign of an imbedded bellmouth nozzle in a turbine cascade inlet section” Subjects and Themes:
- Subjects: ➤ Dimensional analysis - Flow geometry - Nozzle flow - Cascade flow - Three dimensional flow - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL17565512M
- Online Computer Library Center (OCLC) ID: 39708525
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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23Numerical investigations of low-density nozzle flow by solving the Boltzmann equation
By Zheng-Tao Deng
“Numerical investigations of low-density nozzle flow by solving the Boltzmann equation” Metadata:
- Title: ➤ Numerical investigations of low-density nozzle flow by solving the Boltzmann equation
- Author: Zheng-Tao Deng
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - Washington, DC
“Numerical investigations of low-density nozzle flow by solving the Boltzmann equation” Subjects and Themes:
- Subjects: Computational fluid dynamics - Finite difference theory - Boltzman transport equation - Low density flow - Nozzle flow
Edition Identifiers:
- The Open Library ID: OL15411461M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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24Supersonic expansion flow of an ionized gas
By O. Igra
“Supersonic expansion flow of an ionized gas” Metadata:
- Title: ➤ Supersonic expansion flow of an ionized gas
- Author: O. Igra
- Publisher: ➤ Institute for Aerospace Studies
- Publish Date: 1970
- Publish Location: [Downsview, Ont.]
“Supersonic expansion flow of an ionized gas” Subjects and Themes:
- Subjects: Corner flow - Supersonic flow - Ionized gases - Nozzle flow
Edition Identifiers:
- The Open Library ID: OL18931291M
Access and General Info:
- First Year Published: 1970
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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25A comparison of three Navier-Stokes solvers for exhaust nozzle flowfields
By Nicholas J. Georgiadis
“A comparison of three Navier-Stokes solvers for exhaust nozzle flowfields” Metadata:
- Title: ➤ A comparison of three Navier-Stokes solvers for exhaust nozzle flowfields
- Author: Nicholas J. Georgiadis
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 1999
- Publish Location: ➤ [Springfield, Va - [Cleveland, Ohio]
“A comparison of three Navier-Stokes solvers for exhaust nozzle flowfields” Subjects and Themes:
- Subjects: ➤ Exhaust nozzles - Computational grids - Nozzle flow - Flow characteristics - Ejectors - Turbulent mixing - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL15552382M
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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26Computational design aspects of a NASP nozzle/afterbody experiment
By Stephen M. Ruffin
“Computational design aspects of a NASP nozzle/afterbody experiment” Metadata:
- Title: ➤ Computational design aspects of a NASP nozzle/afterbody experiment
- Author: Stephen M. Ruffin
- Number of Pages: Median: 14
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1989
- Publish Location: Washington, D. C
“Computational design aspects of a NASP nozzle/afterbody experiment” Subjects and Themes:
- Subjects: Afterbodies - Aerospace planes - Nozzle flow
Edition Identifiers:
- The Open Library ID: OL19247133M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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27Prediction of temperatures and velocity in a nonequilibrium nozzle flow of air
By Riichi Matsuzaki
“Prediction of temperatures and velocity in a nonequilibrium nozzle flow of air” Metadata:
- Title: ➤ Prediction of temperatures and velocity in a nonequilibrium nozzle flow of air
- Author: Riichi Matsuzaki
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1987
- Publish Location: New York
“Prediction of temperatures and velocity in a nonequilibrium nozzle flow of air” Subjects and Themes:
- Subjects: Nozzle flow
Edition Identifiers:
- The Open Library ID: OL19243813M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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28Three dimensional viscous flow field in an axial flow turbine nozzle passage
By D. Ristiʹc
“Three dimensional viscous flow field in an axial flow turbine nozzle passage” Metadata:
- Title: ➤ Three dimensional viscous flow field in an axial flow turbine nozzle passage
- Author: D. Ristiʹc
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - National Technical Information Service, distributor]
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Three dimensional viscous flow field in an axial flow turbine nozzle passage” Subjects and Themes:
- Subjects: ➤ Viscous flow - Nozzle flow - Axial flow turbines - Cross flow - Three dimensional flow - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL15490460M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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29Numerical analysis of base flowfield for a four-engine clustered nozzle configuration
By Ten-See Wang
“Numerical analysis of base flowfield for a four-engine clustered nozzle configuration” Metadata:
- Title: ➤ Numerical analysis of base flowfield for a four-engine clustered nozzle configuration
- Author: Ten-See Wang
- Language: English
- Publisher: ➤ [National Aeronautics and Space Administration - National Technical Information Service, distributor - American Institute of Aeronautics and Astronautics
- Publish Date: 1995
- Publish Location: ➤ Washington, DC - Springfield, Va
“Numerical analysis of base flowfield for a four-engine clustered nozzle configuration” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Base flow - Turbulent flow - Pressure distribution - Flow distribution - Grid generation (Mathematics) - Multiengine vehicles - Nozzle flow - Base pressure
Edition Identifiers:
- The Open Library ID: OL15542985M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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30Comparison of turbulence models for nozzle-afterbody flows with propulsive jets
By William B. Compton
“Comparison of turbulence models for nozzle-afterbody flows with propulsive jets” Metadata:
- Title: ➤ Comparison of turbulence models for nozzle-afterbody flows with propulsive jets
- Author: William B. Compton
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: Hampton, Va - [Springfield, Va
“Comparison of turbulence models for nozzle-afterbody flows with propulsive jets” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Angle of attack - Axisymmetric flow - Computational fluid dynamics - Convergent-divergent nozzles - Exhaust gases - Free flow - Jet exhaust - K-epsilon turbulence model - Navier-Stokes equation - Nozzle flow - Turbulence models
Edition Identifiers:
- The Open Library ID: OL15504433M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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31Effects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle
By Scott C. Asbury
“Effects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle” Metadata:
- Title: ➤ Effects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle
- Author: Scott C. Asbury
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1999
- Publish Location: Hampton, Va - Springfield, VA
“Effects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle” Subjects and Themes:
- Subjects: ➤ Wind tunnel nozzles - Oblique shock waves - Flow visualization - Boundary layer separation - Nozzle flow - Wind tunnel tests - Convergent-divergent nozzles
Edition Identifiers:
- The Open Library ID: OL15548828M
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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32Fluid spray simulation with two-fluid nozzles
By Robert D. Ingebo
“Fluid spray simulation with two-fluid nozzles” Metadata:
- Title: ➤ Fluid spray simulation with two-fluid nozzles
- Author: Robert D. Ingebo
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service, distributor - NASA
- Publish Date: 1988
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Fluid spray simulation with two-fluid nozzles” Subjects and Themes:
- Subjects: Fuel sprays - Two phase flow - Liquid-solid interfaces - Nozzle flow
Edition Identifiers:
- The Open Library ID: OL15406366M
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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33Analysis of the convergence history of flow through nozzles with shocks
By A. Y. Cheer
“Analysis of the convergence history of flow through nozzles with shocks” Metadata:
- Title: ➤ Analysis of the convergence history of flow through nozzles with shocks
- Author: A. Y. Cheer
- Number of Pages: Median: 629
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1988
- Publish Location: [New York?]
“Analysis of the convergence history of flow through nozzles with shocks” Subjects and Themes:
- Subjects: Convergence - Iterative solution - Nozzle flow
Edition Identifiers:
- The Open Library ID: OL19916836M
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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34The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios
By Kenneth John Kacynski
“The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios” Metadata:
- Title: ➤ The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios
- Author: Kenneth John Kacynski
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios” Subjects and Themes:
- Subjects: ➤ Heat transfer - Thermal diffusion - Nozzle flow - Sweat cooling - Film cooling - Hydrogen oxygen engines - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15404461M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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35Design and checkout of a high speed research nozzle evaluation rig
By Raymond S. Castner
“Design and checkout of a high speed research nozzle evaluation rig” Metadata:
- Title: ➤ Design and checkout of a high speed research nozzle evaluation rig
- Author: Raymond S. Castner
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1997
- Publish Location: ➤ Springfield, VA - [Cleveland, Ohio]
“Design and checkout of a high speed research nozzle evaluation rig” Subjects and Themes:
- Subjects: Evaluation - Design analysis - Scale models - High speed - Nozzle flow
Edition Identifiers:
- The Open Library ID: OL15543119M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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36Radiative interactions in chemically reacting compressible nozzle flows using Monte Carlo simulations
By Jiwen Liu
“Radiative interactions in chemically reacting compressible nozzle flows using Monte Carlo simulations” Metadata:
- Title: ➤ Radiative interactions in chemically reacting compressible nozzle flows using Monte Carlo simulations
- Author: Jiwen Liu
- Language: English
- Publisher: ➤ Institute for Computational and Applied Mechanics, Old Dominion University - NASA Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ Hampton, Va - [Springfield, Va - Norfolk, Va
“Radiative interactions in chemically reacting compressible nozzle flows using Monte Carlo simulations” Subjects and Themes:
- Subjects: ➤ Elliptic Differential equations - Flow distribution - Mathematical models - Monte Carlo method - Navier-Stokes equation - Nozzle flow - Reacting flow
Edition Identifiers:
- The Open Library ID: OL15409429M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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37Effect of delta tabs on free jets from complex nozzles
By K. B. M. Q. Zaman
“Effect of delta tabs on free jets from complex nozzles” Metadata:
- Title: ➤ Effect of delta tabs on free jets from complex nozzles
- Author: K. B. M. Q. Zaman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - Available from NASA Center for Aerospace Information
- Publish Date: 2001
- Publish Location: ➤ [Cleveland, Ohio] - Hanover, MD
“Effect of delta tabs on free jets from complex nozzles” Subjects and Themes:
- Subjects: ➤ Ejectors - Flow distribution - Nozzle flow - Tabs (Control surfaces) - Free jets - Simulation
Edition Identifiers:
- The Open Library ID: OL16048239M
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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38A time-dependent analysis for quasi-one-dimensional nozzle flows with vibrational and chemical nonequilibrium
By John Anderson
“A time-dependent analysis for quasi-one-dimensional nozzle flows with vibrational and chemical nonequilibrium” Metadata:
- Title: ➤ A time-dependent analysis for quasi-one-dimensional nozzle flows with vibrational and chemical nonequilibrium
- Author: John Anderson
- Number of Pages: Median: 30
- Publisher: Naval Ordnance Laboratory
- Publish Date: 1969
- Publish Location: White Oak, Md
“A time-dependent analysis for quasi-one-dimensional nozzle flows with vibrational and chemical nonequilibrium” Subjects and Themes:
- Subjects: Nonequilibrium flow - Nozzle flow
Edition Identifiers:
- The Open Library ID: OL18999734M
Author's Alternative Names:
"John D. Jr Anderson", "Anderson, John David, 1937-....", "約翰·D·安德森", "John D. Anderson curator of Aerodynamics at the National Air and Space Museum at the Smithsonian Institution", "John D. Anderson, Jr.", "Anderson, John David", "جان دی آندرسون", "Anderson, John D. (John David), 1937-", "John D., Jr. Anderson", "Anderson, John D. 1937-", "Anderson, John D. (John David), Jr., 1937-", "John D. Anderson Jr", "Anderson, John David Jr. 1937-", "Anderson, John D., Jr.", "J. D. Anderson", "جون د. أندرسون", "John David Anderson Jr.", "John David ANDERSON", "জন ডি অ্যান্ডারসন", "Anderson, John D., Jr. (John David), 1937-", "约翰 D.安德森", "Anderson, John D. Jr", "جان دی. اندرسون", "约翰·戴维·安德森", "جون د. اندرسون", "John D. Anderson Jr.", "John D Anderson Jr", "约翰·D·安德森", "Anderson, John D. (John David)",Access and General Info:
- First Year Published: 1969
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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39Use of the PARC code to estimate the off-design transonic performance of an over/under turboramjet nozzle
By David W. Lam
“Use of the PARC code to estimate the off-design transonic performance of an over/under turboramjet nozzle” Metadata:
- Title: ➤ Use of the PARC code to estimate the off-design transonic performance of an over/under turboramjet nozzle
- Author: David W. Lam
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Use of the PARC code to estimate the off-design transonic performance of an over/under turboramjet nozzle” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Navier-Stokes equation - Transonic flow - Nozzle geometry - Turboramjet engines - Nozzle efficiency - Nozzle flow - Hypersonic nozzles - Nozzle design
Edition Identifiers:
- The Open Library ID: OL15414400M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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40Kinetic theory model predictions compared with low-thrust axisymmetric nozzle plume data
By B. R. Riley
“Kinetic theory model predictions compared with low-thrust axisymmetric nozzle plume data” Metadata:
- Title: ➤ Kinetic theory model predictions compared with low-thrust axisymmetric nozzle plume data
- Author: B. R. Riley
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1993
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Kinetic theory model predictions compared with low-thrust axisymmetric nozzle plume data” Subjects and Themes:
- Subjects: ➤ Krook equation - Kinetic equations - Gas flow - Kinetic theory - Nozzle flow - Plumes - Mathematical models
Edition Identifiers:
- The Open Library ID: OL15415059M
Access and General Info:
- First Year Published: 1993
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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41Experimental studies of shock-wave/wall-jet interaction in hypersonic flow
By Michael S. Holden
“Experimental studies of shock-wave/wall-jet interaction in hypersonic flow” Metadata:
- Title: ➤ Experimental studies of shock-wave/wall-jet interaction in hypersonic flow
- Author: Michael S. Holden
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1994
- Publish Location: Hampton, Va - [Springfield, Va
“Experimental studies of shock-wave/wall-jet interaction in hypersonic flow” Subjects and Themes:
- Subjects: ➤ Turbulent flow - Hypersonic flow - Wind tunnel tests - Nozzle flow - Film cooling - Wall jets - Shock wave interaction - Shock waves
Edition Identifiers:
- The Open Library ID: OL17000207M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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42An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzles
By Craig A. Hunter
“An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzles” Metadata:
- Title: ➤ An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzles
- Author: Craig A. Hunter
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1995
- Publish Location: Hampton, Va - [Springfield, Va
“An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzles” Subjects and Themes:
- Subjects: ➤ Boundary layer equations - Mathematical models - Performance prediction - Compressible flow - Nozzle efficiency - Nozzle flow - Static thrust - Nozzle design - Convergent-divergent nozzles
Edition Identifiers:
- The Open Library ID: OL15409817M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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43Spreading characteristics and thrust of jets from asymmetric nozzles
By K. B. M. O. Zaman
“Spreading characteristics and thrust of jets from asymmetric nozzles” Metadata:
- Title: ➤ Spreading characteristics and thrust of jets from asymmetric nozzles
- Author: K. B. M. O. Zaman
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Spreading characteristics and thrust of jets from asymmetric nozzles” Subjects and Themes:
- Subjects: ➤ Asymmetry - Axisymmetric flow - Nozzle flow - Sound pressure - Spreading - Tabs (Control surfaces) - Vortices
Edition Identifiers:
- The Open Library ID: OL15423294M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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44Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurations
By Kevin L. Mikkelsen
“Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurations” Metadata:
- Title: ➤ Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurations
- Author: Kevin L. Mikkelsen
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2001
- Publish Location: ➤ [Cleveland, Ohio] - Hanover, MD
“Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurations” Subjects and Themes:
- Subjects: Wind tunnel tests - Cold flow tests - Pressure ratio static tests - Power efficiency - Nozzle flow
Edition Identifiers:
- The Open Library ID: OL16030642M
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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45Nonequilibrium in a low power arcjet nozzle
By Dieter M. Zube
“Nonequilibrium in a low power arcjet nozzle” Metadata:
- Title: ➤ Nonequilibrium in a low power arcjet nozzle
- Author: Dieter M. Zube
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1991
- Publish Location: ➤ [Cleveland, Ohio] - [Springfield, Va
“Nonequilibrium in a low power arcjet nozzle” Subjects and Themes:
- Subjects: ➤ Electron spectroscopy - Nozzle flow - Magnetohydrodynamic flow - Arc jet engines - Plasmas (Physics) - Emission spectra - Absorption spectra
Edition Identifiers:
- The Open Library ID: OL16131193M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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46A survey of the method of characteristics for nonequilibrium, internal flows
By Raymond Sedney
“A survey of the method of characteristics for nonequilibrium, internal flows” Metadata:
- Title: ➤ A survey of the method of characteristics for nonequilibrium, internal flows
- Author: Raymond Sedney
- Publisher: AIAA
- Publish Date: 1969
- Publish Location: New York
“A survey of the method of characteristics for nonequilibrium, internal flows” Subjects and Themes:
- Subjects: Method of characteristics - Nozzle flow
Edition Identifiers:
- The Open Library ID: OL19379595M
Access and General Info:
- First Year Published: 1969
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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47Nozzle flows with coupled vibrational and dissociational nonequilibrium
By Duvvuri Tirumalesa
“Nozzle flows with coupled vibrational and dissociational nonequilibrium” Metadata:
- Title: ➤ Nozzle flows with coupled vibrational and dissociational nonequilibrium
- Author: Duvvuri Tirumalesa
- Number of Pages: Median: 118
- Publisher: ➤ Institute for Aerospace Studies
- Publish Date: 1967
- Publish Location: [Downsview, Ont.]
“Nozzle flows with coupled vibrational and dissociational nonequilibrium” Subjects and Themes:
- Subjects: Hypersonic flow - Nozzle flow
Edition Identifiers:
- The Open Library ID: OL19001516M
Access and General Info:
- First Year Published: 1967
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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48Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application
By Jagdish S. Sokhey
“Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application” Metadata:
- Title: ➤ Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application
- Author: Jagdish S. Sokhey
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - [Cleveland, Ohio]
“Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application” Subjects and Themes:
- Subjects: ➤ Viscous flow - Powered lift aircraft - Vertical landing - Thrust vector control - Exhaust nozzles - Nozzle flow - Analysis (Mathematics)
Edition Identifiers:
- The Open Library ID: OL15539894M
- Online Computer Library Center (OCLC) ID: 40763709
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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