Explore: Hypersonic Flow
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Source: The Open Library
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1High-resolution shock capturing scheme for high Mach number internal flow
By Seokkwan Yoon
“High-resolution shock capturing scheme for high Mach number internal flow” Metadata:
- Title: ➤ High-resolution shock capturing scheme for high Mach number internal flow
- Author: Seokkwan Yoon
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1986
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“High-resolution shock capturing scheme for high Mach number internal flow” Subjects and Themes:
- Subjects: Computational fluid dynamics - High resolution - Hypersonic flow - Mach number - Shock waves
Edition Identifiers:
- The Open Library ID: OL15416509M - OL18082805M - OL14984577M - OL18007657M
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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2Hypersonic pitching-moment shift for stardust reentry capsule forebody
By William A. Wood
“Hypersonic pitching-moment shift for stardust reentry capsule forebody” Metadata:
- Title: ➤ Hypersonic pitching-moment shift for stardust reentry capsule forebody
- Author: William A. Wood
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1997
- Publish Location: Hampton, Va - Springfield, VA
“Hypersonic pitching-moment shift for stardust reentry capsule forebody” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Computational fluid dynamics - Hypersonic flow - Mach number - Navier-Stokes equation - Pitching moments - Space capsules
Edition Identifiers:
- The Open Library ID: OL17582192M - OL18137055M - OL15554563M - OL17132065M
- Online Computer Library Center (OCLC) ID: 41618396
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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3Shock-tunnel combustor testing for hypersonic vehicles
By Mark Loomis
“Shock-tunnel combustor testing for hypersonic vehicles” Metadata:
- Title: ➤ Shock-tunnel combustor testing for hypersonic vehicles
- Author: Mark Loomis
- Language: English
- Publisher: ➤ MCAT Institute - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ Springfield, Va - San Jose, Calif - [Washington, DC
“Shock-tunnel combustor testing for hypersonic vehicles” Subjects and Themes:
- Subjects: ➤ Wind tunnel tests - Two dimensional flow - Hypersonic flow - Supersonic combustion ramjet engines - Propulsion system performance - Propulsion system configurations - Engine tests - Air breathing engines - Hypersonic speed - Combustion chambers - Hypersonic aircraft - Hypersonic inlets - Inlet nozzles - Mach number
Edition Identifiers:
- The Open Library ID: OL17001315M - OL18076085M - OL15403346M
- Online Computer Library Center (OCLC) ID: 32198098
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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4In-flight imaging of transverse gas jets injected into transonic and supersonic crossflows
By Kon-Sheng Charles Wang
“In-flight imaging of transverse gas jets injected into transonic and supersonic crossflows” Metadata:
- Title: ➤ In-flight imaging of transverse gas jets injected into transonic and supersonic crossflows
- Author: Kon-Sheng Charles Wang
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility - National Technical Information Service, distributor]
- Publish Date: 1994
- Publish Location: ➤ Edwards, Calif - [Springfield, Va
“In-flight imaging of transverse gas jets injected into transonic and supersonic crossflows” Subjects and Themes:
- Subjects: ➤ Cross flow - Flight test vehicles - Flow visualization - Gas injection - Hypersonic flow - Imaging techniques - Supersonic flow
Edition Identifiers:
- The Open Library ID: OL15408546M - OL18078619M - OL17005135M
- Online Computer Library Center (OCLC) ID: 32668590
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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5The stability of two-dimensional wakes and shear-layers at high Mach numbers
By D. T. Papageorgiou
“The stability of two-dimensional wakes and shear-layers at high Mach numbers” Metadata:
- Title: ➤ The stability of two-dimensional wakes and shear-layers at high Mach numbers
- Author: D. T. Papageorgiou
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1990
- Publish Location: Hampton, Va
“The stability of two-dimensional wakes and shear-layers at high Mach numbers” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Inviscid flow - Shear layers - Wakes - Two dimensional flow - Hypersonic flow - Laminar flow - Flow stability - High Reynolds number - Mach number
Edition Identifiers:
- The Open Library ID: OL18263144M - OL16137874M - OL17631976M
- Online Computer Library Center (OCLC) ID: 67124982
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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6Rocket-based combined cycle engine technology development
By J. R. DeBonis
“Rocket-based combined cycle engine technology development” Metadata:
- Title: ➤ Rocket-based combined cycle engine technology development
- Author: J. R. DeBonis
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center, Ohio Aerospace Institute, Institute for Computational Mechanics in Propulsion - National Aeronautics and Space Administration, distributor]
- Publish Date: 1996
- Publish Location: ➤ [Cleveland, Ohio] - [Springfield, Va
“Rocket-based combined cycle engine technology development” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Computational grids - Engine inlets - Flow distribution - Hypersonic flow - Navier-Stokes equation - Pressure distribution - Rocket engine design - Rocket engines - Static pressure
Edition Identifiers:
- The Open Library ID: OL17593984M - OL18121288M - OL15504564M
- Online Computer Library Center (OCLC) ID: 41375980
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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7High-order polynomial expansions (HOPE) for flux-vector splitting
By M. S. Liou
“High-order polynomial expansions (HOPE) for flux-vector splitting” Metadata:
- Title: ➤ High-order polynomial expansions (HOPE) for flux-vector splitting
- Author: M. S. Liou
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1991
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“High-order polynomial expansions (HOPE) for flux-vector splitting” Subjects and Themes:
- Subjects: ➤ Viscous flow - Hypersonic flow - Polynomials - Navier-Stokes equation - Supersonic boundary layers - Conical flow - Flux vector splitting - Shock waves
Edition Identifiers:
- The Open Library ID: OL17114482M - OL15407296M - OL18078165M
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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8An upwind-biased, point-implicit relaxation algorithm for viscous, compressible perfect-gas flows
By Peter A. Gnoffo
“An upwind-biased, point-implicit relaxation algorithm for viscous, compressible perfect-gas flows” Metadata:
- Title: ➤ An upwind-biased, point-implicit relaxation algorithm for viscous, compressible perfect-gas flows
- Author: Peter A. Gnoffo
- Language: English
- Number of Pages: Median: 68
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - Langley Research Center - For sale by the National Technical Information Service]
- Publish Date: 1990
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, DC]
“An upwind-biased, point-implicit relaxation algorithm for viscous, compressible perfect-gas flows” Subjects and Themes:
- Subjects: Hypersonic flow - Fluid mechanics
Edition Identifiers:
- The Open Library ID: OL15279381M - OL19380458M - OL18030436M
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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9Low-speed, high-lift aerodynamic characteristics of slender, hypersonic accelerator-type configurations
By Gregory M. Gatlin
“Low-speed, high-lift aerodynamic characteristics of slender, hypersonic accelerator-type configurations” Metadata:
- Title: ➤ Low-speed, high-lift aerodynamic characteristics of slender, hypersonic accelerator-type configurations
- Author: Gregory M. Gatlin
- Language: English
- Number of Pages: Median: 43
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - Langley Research Center - For sale by the National Technical Information Service]
- Publish Date: 1989
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, D.C.]
“Low-speed, high-lift aerodynamic characteristics of slender, hypersonic accelerator-type configurations” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Aerospace planes - Body-wing configurations - Hypersonic flow - Hypersonic planes - Lift (Aerodynamics) - Lift - Aircraft design
Edition Identifiers:
- The Open Library ID: OL19380187M - OL18263011M - OL16137788M
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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10Special course on shock-wave/boundary-layer interactions in supersonic and hypersonic flows
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
“Special course on shock-wave/boundary-layer interactions in supersonic and hypersonic flows” Metadata:
- Title: ➤ Special course on shock-wave/boundary-layer interactions in supersonic and hypersonic flows
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
- Language: English
- Number of Pages: Median: 298
- Publisher: AGARD
- Publish Date: 1993
- Publish Location: ➤ Neuilly-sur-Seine - Neuilly-sur-Seine, France
“Special course on shock-wave/boundary-layer interactions in supersonic and hypersonic flows” Subjects and Themes:
- Subjects: ➤ Hypersonic flow - Shock-boundary layer interaction - Supersonic flow
Edition Identifiers:
- The Open Library ID: OL20259070M - OL19917512M
- All ISBNs: 9789283507185 - 9283507185
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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11Special course on three-dimensional supersonic/hypersonic flows including separation
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
“Special course on three-dimensional supersonic/hypersonic flows including separation” Metadata:
- Title: ➤ Special course on three-dimensional supersonic/hypersonic flows including separation
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
- Language: English
- Number of Pages: Median: 394
- Publisher: AGARD
- Publish Date: 1990
- Publish Location: ➤ Neuilly-sur-Seine - Neuilly sur Seine, France
“Special course on three-dimensional supersonic/hypersonic flows including separation” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL20124782M - OL21039442M
- All ISBNs: 9789283505372 - 9283505379
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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12On the instability of hypersonic flow past a wedge
By Stephen J. Cowley
“On the instability of hypersonic flow past a wedge” Metadata:
- Title: ➤ On the instability of hypersonic flow past a wedge
- Author: Stephen J. Cowley
- Language: English
- Number of Pages: Median: 42
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - ICASE
- Publish Date: 1988 - 1989
- Publish Location: Hampton, Va
“On the instability of hypersonic flow past a wedge” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL15290638M - OL18928898M
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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13Hypersonic flows as related to the national aerospace plane
By Marvin Kussoy
“Hypersonic flows as related to the national aerospace plane” Metadata:
- Title: ➤ Hypersonic flows as related to the national aerospace plane
- Author: Marvin Kussoy
- Language: English
- Number of Pages: Median: 57
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - Eloret Institute - For sale by the National Technical Information Service
- Publish Date: 1991 - 1995
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif - Sunnyvale, Calif
“Hypersonic flows as related to the national aerospace plane” Subjects and Themes:
- Subjects: ➤ Hypersonic flow - Aerospace planes - Computational fluid dynamics - Boundary layers - Flow measurement - Turbulence models - Flow distribution - Hypersonic speed - Wind tunnel tests - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15419808M - OL19243299M
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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14Filtered Rayleigh scattering measurements in supersonic/hypersonic facilities
By Richard B. Miles
“Filtered Rayleigh scattering measurements in supersonic/hypersonic facilities” Metadata:
- Title: ➤ Filtered Rayleigh scattering measurements in supersonic/hypersonic facilities
- Author: Richard B. Miles
- Number of Pages: Median: 10
- Publisher: AIAA
- Publish Date: 1992
- Publish Location: Washington
“Filtered Rayleigh scattering measurements in supersonic/hypersonic facilities” Subjects and Themes:
- Subjects: Hypersonic flow - Rayleigh scattering
Edition Identifiers:
- The Open Library ID: OL19247436M
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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15Computational aeroheating predictions for X-34
By William L. Kleb
“Computational aeroheating predictions for X-34” Metadata:
- Title: ➤ Computational aeroheating predictions for X-34
- Author: William L. Kleb
- Language: English
- Publisher: ➤ American Institute of Aeronautics and Astronautics - National Aeronautics and Space Administration - National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1998
- Publish Location: ➤ Springfield, Va - Hampton, Va - [Washington, DC - [Springfield, Va - Reston, VA
“Computational aeroheating predictions for X-34” Subjects and Themes:
- Subjects: ➤ Aerodynamic heating - Aerothermodynamics - Computational fluid dynamics - Flow distribution - Heat transfer - Hypersonic flow - Navier-Stokes equation - Reynolds averaging - Surface temperature - Upwind schemes (Mathematics) - X-34 reusable launch vehicle
Edition Identifiers:
- The Open Library ID: OL15509418M - OL17134588M
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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16Development of an upwind, finite-volume code with finite-rate chemistry
By Gregory A. Molvik
“Development of an upwind, finite-volume code with finite-rate chemistry” Metadata:
- Title: ➤ Development of an upwind, finite-volume code with finite-rate chemistry
- Author: Gregory A. Molvik
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - MCAT Institute - National Aeronautics and Space Administration
- Publish Date: 1994 - 1995
- Publish Location: ➤ San Jose, CA - Springfield, Va - [Washington, DC - [Washington, D.C
“Development of an upwind, finite-volume code with finite-rate chemistry” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Viscous flow - TVD schemes - Three dimensional bodies - Reacting flow - Upwind schemes (Mathematics) - Engine airframe integration - Hypersonic flow - Supersonic flow - Finite volume method - Finite difference theory - Gases - Algorithms - Computer programs - Hypersonic vehicles
Edition Identifiers:
- The Open Library ID: OL15413734M - OL15381561M
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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17Laminar and turbulent flow computations of type IV shock-shock interference aerothermal loads using unstructured grids
By Guruaja R. Vemaganti
“Laminar and turbulent flow computations of type IV shock-shock interference aerothermal loads using unstructured grids” Metadata:
- Title: ➤ Laminar and turbulent flow computations of type IV shock-shock interference aerothermal loads using unstructured grids
- Author: Guruaja R. Vemaganti
- 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
“Laminar and turbulent flow computations of type IV shock-shock interference aerothermal loads using unstructured grids” Subjects and Themes:
- Subjects: ➤ Turbulent flow - Hypersonic flow - Turbulence models - Thermal stresses - Laminar flow - Aerothermodynamics - Shock layers - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL17790648M - OL15409142M
- Online Computer Library Center (OCLC) ID: 32712246
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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18On the Görtler instability in hypersonic flows
By Y. B. Fu
“On the Görtler instability in hypersonic flows” Metadata:
- Title: ➤ On the Görtler instability in hypersonic flows
- Author: Y. B. Fu
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering
- Publish Date: 1990
- Publish Location: Hampton, Va - [Springfield, Va
“On the Görtler instability in hypersonic flows” Subjects and Themes:
- Subjects: ➤ Gas dissociation - Goertler instability - Hypersonic flow - Ideal gas - Incompressible boundary layer - Real Gases - Transition flow - Vortices
Edition Identifiers:
- The Open Library ID: OL16130442M - OL18245149M
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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19Optimum shape of a blunt forebody in hypersonic flow
By L. Maestrello
“Optimum shape of a blunt forebody in hypersonic flow” Metadata:
- Title: ➤ Optimum shape of a blunt forebody in hypersonic flow
- Author: L. Maestrello
- Language: English
- Publisher: NASA Langley Research Center
- Publish Date: 1989
- Publish Location: Hampton, Va
“Optimum shape of a blunt forebody in hypersonic flow” Subjects and Themes:
- Subjects: ➤ Aerodynamic heating - Blunt bodies - Flow distribution - Forebodies - Hypersonic flow - Newton theory - Wave drag
Edition Identifiers:
- The Open Library ID: OL16122124M - OL17631952M
- Online Computer Library Center (OCLC) ID: 57932749
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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20The use of self-calibrating catalytic probes to measure free-stream atom concentration in a hypersonic flow
By N. M. Reddy
“The use of self-calibrating catalytic probes to measure free-stream atom concentration in a hypersonic flow” Metadata:
- Title: ➤ The use of self-calibrating catalytic probes to measure free-stream atom concentration in a hypersonic flow
- Author: N. M. Reddy
- Publisher: ➤ [Institute for Aerospace Studies] - Institute for Aerospace Studies
- Publish Date: 1966
- Publish Location: [Downsview, Ont.]
“The use of self-calibrating catalytic probes to measure free-stream atom concentration in a hypersonic flow” Subjects and Themes:
- Subjects: ➤ Heat transfer - Hypersonic flow - Catalytic activity - Stagnation point - Atom concentration - Probes
Edition Identifiers:
- The Open Library ID: OL19001484M - OL20986419M
Access and General Info:
- First Year Published: 1966
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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21Integral methods in compressible laminar boundary layers and their application to hypersonic pressure interactions
By Y. Y. Chan
“Integral methods in compressible laminar boundary layers and their application to hypersonic pressure interactions” Metadata:
- Title: ➤ Integral methods in compressible laminar boundary layers and their application to hypersonic pressure interactions
- Author: Y. Y. Chan
- Number of Pages: Median: 49
- Publisher: ➤ Institute for Aerospace Studies - [Institute for Aerospace Studies]
- Publish Date: 1965
- Publish Location: [Downsview, Ont.]
“Integral methods in compressible laminar boundary layers and their application to hypersonic pressure interactions” Subjects and Themes:
- Subjects: Axisymmetric flow - Compressible boundary layer - Hypersonic flow - Laminar boundary flow - Laminar boundary layer
Edition Identifiers:
- The Open Library ID: OL20897787M - OL20986487M
Access and General Info:
- First Year Published: 1965
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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22Turbulence modeling for hypersonic flows
By Joseph G. Marvin
“Turbulence modeling for hypersonic flows” Metadata:
- Title: ➤ Turbulence modeling for hypersonic flows
- Author: Joseph G. Marvin
- Number of Pages: Median: 47
- Publisher: NASA Ames Research Center
- Publish Date: 1989
- Publish Location: [Moffett Field, Calif.]
“Turbulence modeling for hypersonic flows” Subjects and Themes:
- Subjects: Hypersonic flow - Turbulence models
Edition Identifiers:
- The Open Library ID: OL19379746M
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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23Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7
By Don E. Avery
“Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7” Metadata:
- Title: ➤ Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7
- Author: Don E. Avery
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
- Publish Date: 1985
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7” Subjects and Themes:
- Subjects: ➤ Cold surfaces - Heat shielding - Hypersonic flow - Impingement - Reusable heat shielding - Thermal protection - Tiles - Turbulent boundary layer - Turbulent flow
Edition Identifiers:
- The Open Library ID: OL17724417M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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Downloads Are Not Available:
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24Computational, theoretical, and experimental investigation of flow over a sharp flat plate, M1 = 10 - 25
By Henry T. Nagamatsu
“Computational, theoretical, and experimental investigation of flow over a sharp flat plate, M1 = 10 - 25” Metadata:
- Title: ➤ Computational, theoretical, and experimental investigation of flow over a sharp flat plate, M1 = 10 - 25
- Author: Henry T. Nagamatsu
- Number of Pages: Median: 14
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1994
- Publish Location: Washington, D. C
“Computational, theoretical, and experimental investigation of flow over a sharp flat plate, M1 = 10 - 25” Subjects and Themes:
- Subjects: ➤ Hypersonic flow - Shock-boundary layer interaction
Edition Identifiers:
- The Open Library ID: OL19755504M
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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25Temperature measurements in hypersonic air flows using laser-induced O2 fluorescence
By Gabriel Laufer
“Temperature measurements in hypersonic air flows using laser-induced O2 fluorescence” Metadata:
- Title: ➤ Temperature measurements in hypersonic air flows using laser-induced O2 fluorescence
- Author: Gabriel Laufer
- Publisher: ➤ [American Institute of Aeronautics and Astronautics]
- Publish Date: 1988
- Publish Location: [New York]
“Temperature measurements in hypersonic air flows using laser-induced O2 fluorescence” Subjects and Themes:
- Subjects: Hypersonic flow - Laser induced fluorescence - Temperature measurement
Edition Identifiers:
- The Open Library ID: OL19245171M
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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26Prediction of L/D curves for a misssile in hypersonic flow
By Clark, James W.
“Prediction of L/D curves for a misssile in hypersonic flow” Metadata:
- Title: ➤ Prediction of L/D curves for a misssile in hypersonic flow
- Author: Clark, James W.
- Number of Pages: Median: 103
- Publisher: ➤ Massachusetts Institute of Technology
- Publish Date: 1957
- Publish Location: Cambridge, Mass
“Prediction of L/D curves for a misssile in hypersonic flow” Subjects and Themes:
- Subjects: Hypersonic flow - Lift drag ratio
Edition Identifiers:
- The Open Library ID: OL19007458M
Access and General Info:
- First Year Published: 1957
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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27Electron-beam diagnostic methods for hypersonic flow diagnostics
“Electron-beam diagnostic methods for hypersonic flow diagnostics” Metadata:
- Title: ➤ Electron-beam diagnostic methods for hypersonic flow diagnostics
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Electron-beam diagnostic methods for hypersonic flow diagnostics” Subjects and Themes:
- Subjects: Electron beams - Hypersonic flow - Flow measurement - Fluorescence - Flow distribution
Edition Identifiers:
- The Open Library ID: OL17543215M
- Online Computer Library Center (OCLC) ID: 38732798
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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28Development of a method of analysis and computer program for calculating the inviscid flow about the windward surfaces of space shuttle configurations at large angles of attack
By Stephen H. Maslen
“Development of a method of analysis and computer program for calculating the inviscid flow about the windward surfaces of space shuttle configurations at large angles of attack” Metadata:
- Title: ➤ Development of a method of analysis and computer program for calculating the inviscid flow about the windward surfaces of space shuttle configurations at large angles of attack
- Author: Stephen H. Maslen
- Number of Pages: Median: 21
- Publisher: Langley Research Center
- Publish Date: 1974
- Publish Location: Hampton, Va
“Development of a method of analysis and computer program for calculating the inviscid flow about the windward surfaces of space shuttle configurations at large angles of attack” Subjects and Themes:
- Subjects: Inviscid flow - Hypersonic flow - Space shuttles
Edition Identifiers:
- The Open Library ID: OL21499890M
Access and General Info:
- First Year Published: 1974
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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29Inviscid flow about blunted cones of large opening angle at angle of attack
By Stephen H. Maslen
“Inviscid flow about blunted cones of large opening angle at angle of attack” Metadata:
- Title: ➤ Inviscid flow about blunted cones of large opening angle at angle of attack
- Author: Stephen H. Maslen
- Number of Pages: Median: 14
- Publisher: Langley Research Center
- Publish Date: 1975
- Publish Location: Hampton, Va
“Inviscid flow about blunted cones of large opening angle at angle of attack” Subjects and Themes:
- Subjects: Inviscid flow - Hypersonic flow
Edition Identifiers:
- The Open Library ID: OL21499884M
Access and General Info:
- First Year Published: 1975
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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30Perspectives on hypersonic viscous and nonequilibrium flow research
By H. K. Cheng
“Perspectives on hypersonic viscous and nonequilibrium flow research” Metadata:
- Title: ➤ Perspectives on hypersonic viscous and nonequilibrium flow research
- Author: H. K. Cheng
- Number of Pages: Median: 33
- Publisher: ➤ University of Southern California, Dept. of Aerospace Engineering
- Publish Date: 1992
- Publish Location: Los Angeles, Calif
“Perspectives on hypersonic viscous and nonequilibrium flow research” Subjects and Themes:
- Subjects: Hypersonic flow
Edition Identifiers:
- The Open Library ID: OL20272155M
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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31Computational analysis of hypersonic flows past generalized cone-derived waveriders
By Xiaohai He
“Computational analysis of hypersonic flows past generalized cone-derived waveriders” Metadata:
- Title: ➤ Computational analysis of hypersonic flows past generalized cone-derived waveriders
- Author: Xiaohai He
- Number of Pages: Median: 193
- Publisher: University of Oklahoma
- Publish Date: 1992
- Publish Location: Norman, Oklahoma
“Computational analysis of hypersonic flows past generalized cone-derived waveriders” Subjects and Themes:
- Subjects: Computational fluid dynamics - Hypersonic flow - Waveriders
Edition Identifiers:
- The Open Library ID: OL22346760M
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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32Development and validation of an axisymmetric Navier-Stokes solver for hypersonic flows
By R. Broglia
“Development and validation of an axisymmetric Navier-Stokes solver for hypersonic flows” Metadata:
- Title: ➤ Development and validation of an axisymmetric Navier-Stokes solver for hypersonic flows
- Author: R. Broglia
- Number of Pages: Median: 43
- Publisher: ➤ von Karman Institute for Fluid Dynamics
- Publish Date: 1995
- Publish Location: Rhode Saint Genese, Belgium
“Development and validation of an axisymmetric Navier-Stokes solver for hypersonic flows” Subjects and Themes:
- Subjects: Navier Stokes equation - Hypersonic flow
Edition Identifiers:
- The Open Library ID: OL22347239M
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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33Planar laser induced fluorescence measurements and heat transfer measurements in hypersonic air flow
By P. E. Cassady
“Planar laser induced fluorescence measurements and heat transfer measurements in hypersonic air flow” Metadata:
- Title: ➤ Planar laser induced fluorescence measurements and heat transfer measurements in hypersonic air flow
- Author: P. E. Cassady
- Number of Pages: Median: 14
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1991
- Publish Location: Washington
“Planar laser induced fluorescence measurements and heat transfer measurements in hypersonic air flow” Subjects and Themes:
- Subjects: Hypersonic flow - Heat transfer - Laser induced fluorescence
Edition Identifiers:
- The Open Library ID: OL21378495M
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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34Condensation in hypersonic nitrogen wind tunnels
By Melissa A. Lederer
“Condensation in hypersonic nitrogen wind tunnels” Metadata:
- Title: ➤ Condensation in hypersonic nitrogen wind tunnels
- Author: Melissa A. Lederer
- Number of Pages: Median: 15
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1990
- Publish Location: Washington
“Condensation in hypersonic nitrogen wind tunnels” Subjects and Themes:
- Subjects: Hypersonic flow - Condensation - Hypersonic nozzles
Edition Identifiers:
- The Open Library ID: OL21378531M
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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35Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream
By George C. Olsen
“Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream” Metadata:
- Title: ➤ Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream
- Author: George C. Olsen
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream” Subjects and Themes:
- Subjects: ➤ Hypersonic flow - Cold flow tests - Free flow - Supersonic combustion ramjet engines - Film cooling - Mass flow rate - Coolants - Oblique shock waves - Thermal protection - Gas flow - Two dimensional models - Hydrogen - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15416715M
Access and General Info:
- First Year Published: 1995
- 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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36Numerical simulation of shock-induced combustion generated by high-speed projectiles in detonable gas mixtures
By Shaye Yungster
“Numerical simulation of shock-induced combustion generated by high-speed projectiles in detonable gas mixtures” Metadata:
- Title: ➤ Numerical simulation of shock-induced combustion generated by high-speed projectiles in detonable gas mixtures
- Author: Shaye Yungster
- Number of Pages: Median: 14
- Publisher: AIAA
- Publish Date: 1989
- Publish Location: New York
“Numerical simulation of shock-induced combustion generated by high-speed projectiles in detonable gas mixtures” Subjects and Themes:
- Subjects: Hypersonic flow - Combustion
Edition Identifiers:
- The Open Library ID: OL22344809M
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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37A new parabolized Navier-Stokes code for chemically reacting flow fields
By Dinesh Kumble Prabhu
“A new parabolized Navier-Stokes code for chemically reacting flow fields” Metadata:
- Title: ➤ A new parabolized Navier-Stokes code for chemically reacting flow fields
- Author: Dinesh Kumble Prabhu
- Number of Pages: Median: 106
- Publisher: Iowa State University
- Publish Date: 1987
- Publish Location: Ames, Iowa
“A new parabolized Navier-Stokes code for chemically reacting flow fields” Subjects and Themes:
- Subjects: Hypersonic flow - Aerothermodynamics - Chemical reactions - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL18926612M
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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38Multigrid for hypersonic viscous two- and three-dimensional flows
By Eli Turkel
“Multigrid for hypersonic viscous two- and three-dimensional flows” Metadata:
- Title: ➤ Multigrid for hypersonic viscous two- and three-dimensional flows
- Author: Eli Turkel
- Number of Pages: Median: 21
- Publisher: ➤ Institute for Computer Applications in Science and Engineering
- Publish Date: 1991
- Publish Location: Hampton, Va
“Multigrid for hypersonic viscous two- and three-dimensional flows” Subjects and Themes:
- Subjects: Multigrid methods - Hypersonic flow - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL21499531M
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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39A statistical theory for gas surface interactions in rarefied hypersonic flows
By A. A. Agbormbai
“A statistical theory for gas surface interactions in rarefied hypersonic flows” Metadata:
- Title: ➤ A statistical theory for gas surface interactions in rarefied hypersonic flows
- Author: A. A. Agbormbai
- Number of Pages: Median: 45
- Publisher: ➤ Imperial College of Science and Technology, Dept. of Aeronautics
- Publish Date: 1988
- Publish Location: [London]
“A statistical theory for gas surface interactions in rarefied hypersonic flows” Subjects and Themes:
- Subjects: Hypersonic flow - Gas-surface interactions
Edition Identifiers:
- The Open Library ID: OL18927098M
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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40Numerical simulation of hypersonic flow around a space plane. I
By Yukimitsu Yamamoto
“Numerical simulation of hypersonic flow around a space plane. I” Metadata:
- Title: ➤ Numerical simulation of hypersonic flow around a space plane. I
- Author: Yukimitsu Yamamoto
- Number of Pages: Median: 21
- Publisher: National Aerospace Laboratory
- Publish Date: 1988
- Publish Location: Tokyo
“Numerical simulation of hypersonic flow around a space plane. I” Subjects and Themes:
- Subjects: Hypersonic flow - Aerospace planes
Edition Identifiers:
- The Open Library ID: OL18928639M
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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41Numerical simulation of hypersonic flow around a space plane. II. Application to high angles of attack flow
By Yukimitsu Yamamoto
“Numerical simulation of hypersonic flow around a space plane. II. Application to high angles of attack flow” Metadata:
- Title: ➤ Numerical simulation of hypersonic flow around a space plane. II. Application to high angles of attack flow
- Author: Yukimitsu Yamamoto
- Number of Pages: Median: 20
- Publisher: National Aerospace Laboratory
- Publish Date: 1989
- Publish Location: Chofu, Tokyo, Japan
“Numerical simulation of hypersonic flow around a space plane. II. Application to high angles of attack flow” Subjects and Themes:
- Subjects: Hypersonic flow - Aerospace planes
Edition Identifiers:
- The Open Library ID: OL19380211M
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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42Numerical simulation of hypersonic flow around a space plane. III Analysis of aerothermodynamic heating
By Yukimitsu Yamamoto
“Numerical simulation of hypersonic flow around a space plane. III Analysis of aerothermodynamic heating” Metadata:
- Title: ➤ Numerical simulation of hypersonic flow around a space plane. III Analysis of aerothermodynamic heating
- Author: Yukimitsu Yamamoto
- Number of Pages: Median: 28
- Publisher: National Aerospace Laboratory
- Publish Date: 1989
- Publish Location: Tokyo
“Numerical simulation of hypersonic flow around a space plane. III Analysis of aerothermodynamic heating” Subjects and Themes:
- Subjects: Hypersonic flow - Aerothermodynamics - Aerospace planes
Edition Identifiers:
- The Open Library ID: OL20966794M
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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43Design and testing of an axisymmetric flow nozzle for Mach number seven
By K. R. Enkenhus
“Design and testing of an axisymmetric flow nozzle for Mach number seven” Metadata:
- Title: ➤ Design and testing of an axisymmetric flow nozzle for Mach number seven
- Author: K. R. Enkenhus
- Number of Pages: Median: 27
- Publisher: Institute of Aerophysics
- Publish Date: 1955
- Publish Location: [Downsview, Ont.]
“Design and testing of an axisymmetric flow nozzle for Mach number seven” Subjects and Themes:
- Subjects: Nozzles - Hypersonic flow
Edition Identifiers:
- The Open Library ID: OL20968422M
Access and General Info:
- First Year Published: 1955
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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44Prediction of two-dimensional time-dependent gasdynamic flows for hypersonic studies
By D. F. Hawken
“Prediction of two-dimensional time-dependent gasdynamic flows for hypersonic studies” Metadata:
- Title: ➤ Prediction of two-dimensional time-dependent gasdynamic flows for hypersonic studies
- Author: D. F. Hawken
- Publisher: ➤ Institute for Aerospace Studies
- Publish Date: 1990
- Publish Location: Downsview, Ont
“Prediction of two-dimensional time-dependent gasdynamic flows for hypersonic studies” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL20966721M
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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45Analogue networks for high heat-transfer rate measurements
By Z. A. Walenta
“Analogue networks for high heat-transfer rate measurements” Metadata:
- Title: ➤ Analogue networks for high heat-transfer rate measurements
- Author: Z. A. Walenta
- Number of Pages: Median: 34
- Publisher: ➤ Institute for Aerospace Studies
- Publish Date: 1964
- Publish Location: [Downsview, Ont.]
“Analogue networks for high heat-transfer rate measurements” Subjects and Themes:
- Subjects: Hypersonic flow - Heat transfer - Stagnation point
Edition Identifiers:
- The Open Library ID: OL19045896M
Access and General Info:
- First Year Published: 1964
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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46An investigation of hypersonic shock tunnel testing at an equilibrium interface condition of 4,100K: theory and experiment
By Marco A. S. Minucci
“An investigation of hypersonic shock tunnel testing at an equilibrium interface condition of 4,100K: theory and experiment” Metadata:
- Title: ➤ An investigation of hypersonic shock tunnel testing at an equilibrium interface condition of 4,100K: theory and experiment
- Author: Marco A. S. Minucci
- Number of Pages: Median: 17
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1991
- Publish Location: Washington, D. C
“An investigation of hypersonic shock tunnel testing at an equilibrium interface condition of 4,100K: theory and experiment” Subjects and Themes:
- Subjects: Hypersonic flow - Hypersonic shock tubes
Edition Identifiers:
- The Open Library ID: OL21500141M
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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47Improving the performance of the equilibrium interface technique in shock tube flows
By Marco A. S. Minucci
“Improving the performance of the equilibrium interface technique in shock tube flows” Metadata:
- Title: ➤ Improving the performance of the equilibrium interface technique in shock tube flows
- Author: Marco A. S. Minucci
- Number of Pages: Median: 14
- Publisher: Sine nomine
- Publish Date: 1993
- Publish Location: [S.l.]
“Improving the performance of the equilibrium interface technique in shock tube flows” Subjects and Themes:
- Subjects: Hypersonic flow
Edition Identifiers:
- The Open Library ID: OL22347120M
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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48A comparison of Maslen's method, Riley & Dejarnette's method and MacCormack's method in hypersonic inviscid flow
By Gilman Man Yuen Siu
“A comparison of Maslen's method, Riley & Dejarnette's method and MacCormack's method in hypersonic inviscid flow” Metadata:
- Title: ➤ A comparison of Maslen's method, Riley & Dejarnette's method and MacCormack's method in hypersonic inviscid flow
- Author: Gilman Man Yuen Siu
- Number of Pages: Median: 94
- Publisher: ➤ Department of Aerospace Studies, University of Toronto
- Publish Date: 1992
- Publish Location: [Downsview, Ont.]
“A comparison of Maslen's method, Riley & Dejarnette's method and MacCormack's method in hypersonic inviscid flow” Subjects and Themes:
- Subjects: Hypersonic flow
Edition Identifiers:
- The Open Library ID: OL19246211M
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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49The maximum entropy approach applied to energy exchange, chemical reactions and ionisation in the direct simulation Monte Carlo method for rarefied hypersonic flows
By M. A. Gallis
“The maximum entropy approach applied to energy exchange, chemical reactions and ionisation in the direct simulation Monte Carlo method for rarefied hypersonic flows” Metadata:
- Title: ➤ The maximum entropy approach applied to energy exchange, chemical reactions and ionisation in the direct simulation Monte Carlo method for rarefied hypersonic flows
- Author: M. A. Gallis
- Number of Pages: Median: 27
- Publisher: ➤ Imperial College of Science Technology and Medicine
- Publish Date: 1993
- Publish Location: London
“The maximum entropy approach applied to energy exchange, chemical reactions and ionisation in the direct simulation Monte Carlo method for rarefied hypersonic flows” Subjects and Themes:
- Subjects: Hypersonic flow - Maximum entropy method - Monte Carlo method
Edition Identifiers:
- The Open Library ID: OL19917161M
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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50CW laser strategies for simultaneous multi-parameter measurements in high-speed gas flows
By M. D. Di Rosa
“CW laser strategies for simultaneous multi-parameter measurements in high-speed gas flows” Metadata:
- Title: ➤ CW laser strategies for simultaneous multi-parameter measurements in high-speed gas flows
- Author: M. D. Di Rosa
- Number of Pages: Median: 11
- Publisher: AIAA
- Publish Date: 1992
- Publish Location: Washington
“CW laser strategies for simultaneous multi-parameter measurements in high-speed gas flows” Subjects and Themes:
- Subjects: Hypersonic flow - Continuous wave lasers
Edition Identifiers:
- The Open Library ID: OL19247349M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find CW laser strategies for simultaneous multi-parameter measurements in high-speed gas flows at online marketplaces:
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