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Source: The Open Library
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Search results from The Open Library
1Numerical solutions of the complete Navier-Stokes equations
By H. A. Hassan
“Numerical solutions of the complete Navier-Stokes equations” Metadata:
- Title: ➤ Numerical solutions of the complete Navier-Stokes equations
- Author: H. A. Hassan
- Language: English
- Publisher: ➤ Dept. of Mechanical and Aerospace Engineering, North Carolina State University - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1989 - 1994 - 1995 - 1996
- Publish Location: ➤ [Washington, DC - [Washington, D.C - Raleigh, N.C - Springfield, Va
“Numerical solutions of the complete Navier-Stokes equations” Subjects and Themes:
- Subjects: ➤ Navier-Stokes equation - Turbulent flow - Turbulence models - Eddy viscosity - Flow velocity - Supersonic combustion - Mixing layers (Fluids) - Jet flow - Navier-Stokes equations - Compressible flow - Compressibility - Numerical solutions - Turbulent mixing - Computational fluid dynamics - Numerical analysis - Vorticity - Boundary layer separation - Vortices - Pressure gradients - Three dimensional flow - Aerodynamic characteristics - Airfoils
Edition Identifiers:
- The Open Library ID: OL15419184M - OL15452379M - OL16135487M - OL14706079M
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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2Navier-Stokes simulation of the supersonic combustion flowfield in a ram accelerator
By Shaye Yungster
“Navier-Stokes simulation of the supersonic combustion flowfield in a ram accelerator” Metadata:
- Title: ➤ Navier-Stokes simulation of the supersonic combustion flowfield in a ram accelerator
- Author: Shaye Yungster
- Language: English
- Number of Pages: Median: 23
- Publisher: ➤ American Institute for Aeronautics and Astronautics - National Aeronautics and Space Administration - For sale by the National Technical Information Service
- Publish Date: 1991
- Publish Location: ➤ [Springfield, Va - Washington, D. C - [Washington, DC]
“Navier-Stokes simulation of the supersonic combustion flowfield in a ram accelerator” Subjects and Themes:
- Subjects: Navier-Stokes equations - Detonation waves - Ram accelerator - Supersonic combustion - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL15300381M - OL21378513M - OL18035295M - OL17102778M
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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3Fuel-rich catalytic combustion of a high density fuel
By Theodore A. Brabbs
“Fuel-rich catalytic combustion of a high density fuel” Metadata:
- Title: ➤ Fuel-rich catalytic combustion of a high density fuel
- Author: Theodore A. Brabbs
- Language: English
- Number of Pages: Median: 11
- Publisher: ➤ For sale by the National Technical Information Service - Lewis Research Center - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1993
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va - Cleveland, Ohio
“Fuel-rich catalytic combustion of a high density fuel” Subjects and Themes:
- Subjects: ➤ Fuel combustion - Hydrocarbon combustion - Propellant combustion - Supersonic combustion - Hydrocarbon fuels - Combustion control - Combustion products - Catalysis - Catalytic combustion
Edition Identifiers:
- The Open Library ID: OL16125621M - OL19146774M - OL18227608M - OL19916521M
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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4Instrumentation development for study of Reynolds analogy in reacting flows
By Dianne J. DeTurris
“Instrumentation development for study of Reynolds analogy in reacting flows” Metadata:
- Title: ➤ Instrumentation development for study of Reynolds analogy in reacting flows
- Author: Dianne J. DeTurris
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: [Springfield, Va - Hampton, Va
“Instrumentation development for study of Reynolds analogy in reacting flows” Subjects and Themes:
- Subjects: ➤ Friction measurement - Heat transfer - Reacting flow - Skin friction - Strain gages - Supersonic combustion - Supersonic combustion ramjet engines - Supersonic flow - Turbulent boundary layer - Wall flow
Edition Identifiers:
- The Open Library ID: OL15421527M - OL17793730M
- Online Computer Library Center (OCLC) ID: 35218955
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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5Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program
By Alexander S. Roudakov
“Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program” Metadata:
- Title: ➤ Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program
- Author: Alexander S. Roudakov
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ Edwards, Calif - Springfield, VA
“Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program” Subjects and Themes:
- Subjects: ➤ Missiles - Supersonic combustion - Airborne equipment - Hypersonic speed - Supersonic combustion ramjet engines - Flight tests - Launching
Edition Identifiers:
- The Open Library ID: OL17583619M - OL15548793M
- Online Computer Library Center (OCLC) ID: 41942401
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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6Effect of heat release on the spatial stability of a supersonic reacting mixing layer
By Thomas L. Jackson
“Effect of heat release on the spatial stability of a supersonic reacting mixing layer” Metadata:
- Title: ➤ Effect of heat release on the spatial stability of a supersonic reacting mixing layer
- Author: Thomas L. Jackson
- Number of Pages: Median: 10
- Publisher: ICASE
- Publish Date: 1988
- Publish Location: Hampton, Va
“Effect of heat release on the spatial stability of a supersonic reacting mixing layer” Subjects and Themes:
- Subjects: Compressible mixing layer - Stability - Supersonic combustion
Edition Identifiers:
- The Open Library ID: OL18929310M
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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7The aerospace plane design challenge
By Unmeel B. Mehta
“The aerospace plane design challenge” Metadata:
- Title: ➤ The aerospace plane design challenge
- Author: Unmeel B. Mehta
- Language: English
- Publisher: NASA Ames Resarch Center
- Publish Date: 1990
- Publish Location: Moffett Field, Calif
“The aerospace plane design challenge” Subjects and Themes:
- Subjects: Aerospace planes - Computational fluid dynamics - Design analysis - National Aerospace Plane Program - Supersonic combustion
Edition Identifiers:
- The Open Library ID: OL16125227M
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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8Diagnostics in supersonic combustion
By Y. M. Timnat
“Diagnostics in supersonic combustion” Metadata:
- Title: ➤ Diagnostics in supersonic combustion
- Author: Y. M. Timnat
- Publisher: AIAA
- Publish Date: 1987
- Publish Location: New York
“Diagnostics in supersonic combustion” Subjects and Themes:
- Subjects: Supersonic combustion
Edition Identifiers:
- The Open Library ID: OL19250684M
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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9Laser-initiated conical detonation wave for supersonic combustion
By G. Carrier
“Laser-initiated conical detonation wave for supersonic combustion” Metadata:
- Title: ➤ Laser-initiated conical detonation wave for supersonic combustion
- Author: G. Carrier
- Number of Pages: Median: 11
- Publisher: AIAA
- Publish Date: 1991
- Publish Location: New York
“Laser-initiated conical detonation wave for supersonic combustion” Subjects and Themes:
- Subjects: Detonation waves - Supersonic combustion
Edition Identifiers:
- The Open Library ID: OL20779449M
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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10Analytical and experimental study of supersonic combustion of hydrogen in a vitiated airstream
By Marshall C. Burrows
“Analytical and experimental study of supersonic combustion of hydrogen in a vitiated airstream” Metadata:
- Title: ➤ Analytical and experimental study of supersonic combustion of hydrogen in a vitiated airstream
- Author: Marshall C. Burrows
- Number of Pages: Median: 25
- Publisher: Sine nomine
- Publish Date: 1973
- Publish Location: [S.l.]
“Analytical and experimental study of supersonic combustion of hydrogen in a vitiated airstream” Subjects and Themes:
- Subjects: Hydrogen - Supersonic combustion
Edition Identifiers:
- The Open Library ID: OL22346876M
Access and General Info:
- First Year Published: 1973
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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11Annual technical report on turbulent reacting flows and supersonic combustion
By C. T. Bowman
“Annual technical report on turbulent reacting flows and supersonic combustion” Metadata:
- Title: ➤ Annual technical report on turbulent reacting flows and supersonic combustion
- Author: C. T. Bowman
- Number of Pages: Median: 24
- Publisher: ➤ Stanford University, High Temperature Gasdynamics Laboratory
- Publish Date: 1991
- Publish Location: Stanford, Calif
“Annual technical report on turbulent reacting flows and supersonic combustion” Subjects and Themes:
- Subjects: Turbulent flow - Supersonic combustion
Edition Identifiers:
- The Open Library ID: OL21379252M
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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12A laser-induced-fluorescence visualization study of transverse, sonic fuel injection in a nonreacting supersonic combustor
By James C. McDaniel
“A laser-induced-fluorescence visualization study of transverse, sonic fuel injection in a nonreacting supersonic combustor” Metadata:
- Title: ➤ A laser-induced-fluorescence visualization study of transverse, sonic fuel injection in a nonreacting supersonic combustor
- Author: James C. McDaniel
- Publisher: AIAA
- Publish Date: 1986
- Publish Location: New York
“A laser-induced-fluorescence visualization study of transverse, sonic fuel injection in a nonreacting supersonic combustor” Subjects and Themes:
- Subjects: Supersonic combustion
Edition Identifiers:
- The Open Library ID: OL19987350M
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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13Supersonic mixing and combustion of a hydrogen jet in a coaxial high-temperature test gas
By H. L. Beach
“Supersonic mixing and combustion of a hydrogen jet in a coaxial high-temperature test gas” Metadata:
- Title: ➤ Supersonic mixing and combustion of a hydrogen jet in a coaxial high-temperature test gas
- Author: H. L. Beach
- Number of Pages: Median: 10
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1972
- Publish Location: New York
“Supersonic mixing and combustion of a hydrogen jet in a coaxial high-temperature test gas” Subjects and Themes:
- Subjects: Mixing - Supersonic combustion
Edition Identifiers:
- The Open Library ID: OL19751824M
Access and General Info:
- First Year Published: 1972
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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14Analysis of losses in supersonic mixing and reacting flows
By David W. Riggins
“Analysis of losses in supersonic mixing and reacting flows” Metadata:
- Title: ➤ Analysis of losses in supersonic mixing and reacting flows
- Author: David W. Riggins
- Number of Pages: Median: 20
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1991
- Publish Location: Washington, D. C
“Analysis of losses in supersonic mixing and reacting flows” Subjects and Themes:
- Subjects: Mixing - Reacting flow - Supersonic combustion
Edition Identifiers:
- The Open Library ID: OL19752212M
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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15A comparative study of scramjet injection strategies for high Mach number flows
By David W. Riggins
“A comparative study of scramjet injection strategies for high Mach number flows” Metadata:
- Title: ➤ A comparative study of scramjet injection strategies for high Mach number flows
- Author: David W. Riggins
- Number of Pages: Median: 23
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1992
- Publish Location: Washington, D. C
“A comparative study of scramjet injection strategies for high Mach number flows” Subjects and Themes:
- Subjects: Thrust - Injection - Supersonic combustion
Edition Identifiers:
- The Open Library ID: OL19752956M
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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16A numerical study of mixing enhancement in a supersonic combustor
By David W. Riggins
“A numerical study of mixing enhancement in a supersonic combustor” Metadata:
- Title: ➤ A numerical study of mixing enhancement in a supersonic combustor
- Author: David W. Riggins
- Number of Pages: Median: 16
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1990
- Publish Location: Washington, D. C
“A numerical study of mixing enhancement in a supersonic combustor” Subjects and Themes:
- Subjects: Mixing - Fuel injection - Supersonic combustion
Edition Identifiers:
- The Open Library ID: OL19752026M
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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17Heat release effects on mixing in supersonic reacting free shear-layers
By O. H. Planche
“Heat release effects on mixing in supersonic reacting free shear-layers” Metadata:
- Title: ➤ Heat release effects on mixing in supersonic reacting free shear-layers
- Author: O. H. Planche
- Number of Pages: Median: 11
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1992
- Publish Location: Washington, D. C
“Heat release effects on mixing in supersonic reacting free shear-layers” Subjects and Themes:
- Subjects: Mixing layers - Supersonic combustion
Edition Identifiers:
- The Open Library ID: OL19752180M
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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18Noncircular jet dynamics in supersonic combustion
By E. Gutmark
“Noncircular jet dynamics in supersonic combustion” Metadata:
- Title: ➤ Noncircular jet dynamics in supersonic combustion
- Author: E. Gutmark
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1987
- Publish Location: New York
“Noncircular jet dynamics in supersonic combustion” Subjects and Themes:
- Subjects: Mixing - Supersonic combustion
Edition Identifiers:
- The Open Library ID: OL19244595M
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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19Effect of density gradients in confined supersonic shear layers
By Oshin Peroomian
“Effect of density gradients in confined supersonic shear layers” Metadata:
- Title: ➤ Effect of density gradients in confined supersonic shear layers
- Author: Oshin Peroomian
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Effect of density gradients in confined supersonic shear layers” Subjects and Themes:
- Subjects: ➤ Density (Mass/volume) - Supersonic combustion - Mathematical models - Cross flow - Acoustic properties - Combustion chambers - Shear layers - Modes (Standing waves) - Euler equations of motion - Vortex sheets - Three dimensional motion - Supersonic speed - Compressible flow
Edition Identifiers:
- The Open Library ID: OL15418794M
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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20Supersonic combustion of hydrogen injected perpendicular to a ducted vitiated airstream
By R. Clayton Rogers
“Supersonic combustion of hydrogen injected perpendicular to a ducted vitiated airstream” Metadata:
- Title: ➤ Supersonic combustion of hydrogen injected perpendicular to a ducted vitiated airstream
- Author: R. Clayton Rogers
- Number of Pages: Median: 10
- Publisher: AIAA
- Publish Date: 1973
- Publish Location: New York
“Supersonic combustion of hydrogen injected perpendicular to a ducted vitiated airstream” Subjects and Themes:
- Subjects: Hydrogen - Supersonic combustion
Edition Identifiers:
- The Open Library ID: OL20897956M
Access and General Info:
- First Year Published: 1973
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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21Mixing enhancement in a supersonic combustor
By J. Philip Drummond
“Mixing enhancement in a supersonic combustor” Metadata:
- Title: ➤ Mixing enhancement in a supersonic combustor
- Author: J. Philip Drummond
- Number of Pages: Median: 15
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1989
- Publish Location: Washington, D. C
“Mixing enhancement in a supersonic combustor” Subjects and Themes:
- Subjects: Mixing - Supersonic combustion
Edition Identifiers:
- The Open Library ID: OL19752244M
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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22Supersonic reacting internal flow fields
By J. Philip Drummond
“Supersonic reacting internal flow fields” Metadata:
- Title: ➤ Supersonic reacting internal flow fields
- Author: J. Philip Drummond
- Language: English
- Number of Pages: Median: 64
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1990
- Publish Location: ➤ Springfield, Va - [Washington, D.C.?
“Supersonic reacting internal flow fields” Subjects and Themes:
- Subjects: ➤ Aerodynamics, Supersonic - Combustion - Flow distribution - Fluid dynamics (Space environment) - Hypersonic vehicles - Internal flow - Propulsion - Propulsion system performance - Supersonic Aerodynamics - Supersonic combustion - Supersonic combustion ramjet engines - Supersonic flow
Edition Identifiers:
- The Open Library ID: OL15423539M
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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23Vorticity generation by contoured wall injectors
By Ian A. Waitz
“Vorticity generation by contoured wall injectors” Metadata:
- Title: ➤ Vorticity generation by contoured wall injectors
- Author: Ian A. Waitz
- Number of Pages: Median: 16
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1992
- Publish Location: Washington, D. C
“Vorticity generation by contoured wall injectors” Subjects and Themes:
- Subjects: Fuel injection - Vorticity - Supersonic combustion
Edition Identifiers:
- The Open Library ID: OL19752200M
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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24A two-dimensional numerical simulation of shock-enhanced mixing in a rectangular scramjet flowfield with parallel hydrogen injection
By N. D. Domel
“A two-dimensional numerical simulation of shock-enhanced mixing in a rectangular scramjet flowfield with parallel hydrogen injection” Metadata:
- Title: ➤ A two-dimensional numerical simulation of shock-enhanced mixing in a rectangular scramjet flowfield with parallel hydrogen injection
- Author: N. D. Domel
- Number of Pages: Median: 11
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1991
- Publish Location: Washington, D. C
“A two-dimensional numerical simulation of shock-enhanced mixing in a rectangular scramjet flowfield with parallel hydrogen injection” Subjects and Themes:
- Subjects: Mixing - Supersonic combustion
Edition Identifiers:
- The Open Library ID: OL19752222M
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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25Evaluation of parallel injector configurations for supersonic combustion
By G. Burton Northam
“Evaluation of parallel injector configurations for supersonic combustion” Metadata:
- Title: ➤ Evaluation of parallel injector configurations for supersonic combustion
- Author: G. Burton Northam
- Number of Pages: Median: 14
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1989
- Publish Location: Washington, D. C
“Evaluation of parallel injector configurations for supersonic combustion” Subjects and Themes:
- Subjects: Injectors - Supersonic combustion
Edition Identifiers:
- The Open Library ID: OL19752250M
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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26A review of supersonic combustion research at AEDC with hypersonic applications
By Philip M. Rubins
“A review of supersonic combustion research at AEDC with hypersonic applications” Metadata:
- Title: ➤ A review of supersonic combustion research at AEDC with hypersonic applications
- Author: Philip M. Rubins
- Number of Pages: Median: 11
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1993
- Publish Location: Washington, D. C
“A review of supersonic combustion research at AEDC with hypersonic applications” Subjects and Themes:
- Subjects: Supersonic combustion - Hypersonic combustion
Edition Identifiers:
- The Open Library ID: OL19755649M
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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27Planar Rayleigh scattering and laser-induced fluorescence for visualization of a hot, Mach 2 annular air jet
By R. Jeffrey Balla
“Planar Rayleigh scattering and laser-induced fluorescence for visualization of a hot, Mach 2 annular air jet” Metadata:
- Title: ➤ Planar Rayleigh scattering and laser-induced fluorescence for visualization of a hot, Mach 2 annular air jet
- Author: R. Jeffrey Balla
- 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
“Planar Rayleigh scattering and laser-induced fluorescence for visualization of a hot, Mach 2 annular air jet” Subjects and Themes:
- Subjects: ➤ Laser induced fluorescence - Flow measurement - Supersonic combustion - Air jets - Nonintrusive measurement - Rayleigh scattering - Turbulent jets - Flow visualization
Edition Identifiers:
- The Open Library ID: OL15402725M
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:
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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28Ignition delays, heats of combustion, and reaction rates of aluminum alkyl derivatives used as ignition and combustion enhancers for supersonic combustion
By T. W. Ryan
“Ignition delays, heats of combustion, and reaction rates of aluminum alkyl derivatives used as ignition and combustion enhancers for supersonic combustion” Metadata:
- Title: ➤ Ignition delays, heats of combustion, and reaction rates of aluminum alkyl derivatives used as ignition and combustion enhancers for supersonic combustion
- Author: T. W. Ryan
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1992
- Publish Location: ➤ Hampton, Va - [Springfield, Va.?
“Ignition delays, heats of combustion, and reaction rates of aluminum alkyl derivatives used as ignition and combustion enhancers for supersonic combustion” Subjects and Themes:
- Subjects: ➤ Fuel combustion - Pyrophoric materials - Jet engine fuels - Alkyl compounds - Thermochemical properties - Reaction kinetics - Organic aluminum compounds - Supersonic combustion
Edition Identifiers:
- The Open Library ID: OL15405400M
Access and General Info:
- First Year Published: 1992
- 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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29Mixing and combustion enhancement from unsteady shock-fuel layer interactions
By Jean-Luc Cambier
“Mixing and combustion enhancement from unsteady shock-fuel layer interactions” Metadata:
- Title: ➤ Mixing and combustion enhancement from unsteady shock-fuel layer interactions
- Author: Jean-Luc Cambier
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1994
- Publish Location: Washington, D. C
“Mixing and combustion enhancement from unsteady shock-fuel layer interactions” Subjects and Themes:
- Subjects: Mixing - Detonation waves - Supersonic combustion
Edition Identifiers:
- The Open Library ID: OL19001412M
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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30Ignition delay and characteristic reaction length in shock induced supersonic combustion
By T. Gary Yip
“Ignition delay and characteristic reaction length in shock induced supersonic combustion” Metadata:
- Title: ➤ Ignition delay and characteristic reaction length in shock induced supersonic combustion
- Author: T. Gary Yip
- Number of Pages: Median: 10
- Publisher: AIAA
- Publish Date: 1989
- Publish Location: New York
“Ignition delay and characteristic reaction length in shock induced supersonic combustion” Subjects and Themes:
- Subjects: Supersonic combustion
Edition Identifiers:
- The Open Library ID: OL19379835M
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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31An analytical and computational investigation of shock-induced vortical flows with applications to supersonic combustion
By Joseph Yang
“An analytical and computational investigation of shock-induced vortical flows with applications to supersonic combustion” Metadata:
- Title: ➤ An analytical and computational investigation of shock-induced vortical flows with applications to supersonic combustion
- Author: Joseph Yang
- Number of Pages: Median: 347
- Publisher: ➤ California Institute of Technology
- Publish Date: 1991
- Publish Location: Pasadena, Calif
“An analytical and computational investigation of shock-induced vortical flows with applications to supersonic combustion” Subjects and Themes:
- Subjects: Vortical flow - Supersonic combustion - Shock-induced combustion
Edition Identifiers:
- The Open Library ID: OL19002265M
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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32Progress toward shock enhancement of supersonic combustion processes
By Frank E. Marble
“Progress toward shock enhancement of supersonic combustion processes” Metadata:
- Title: ➤ Progress toward shock enhancement of supersonic combustion processes
- Author: Frank E. Marble
- Publisher: AIAA
- Publish Date: 1987
- Publish Location: New York
“Progress toward shock enhancement of supersonic combustion processes” Subjects and Themes:
- Subjects: Supersonic combustion
Edition Identifiers:
- The Open Library ID: OL19250595M
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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33Preliminary calibration of a generic scramjet combustor
By P. A. Jacobs
“Preliminary calibration of a generic scramjet combustor” Metadata:
- Title: ➤ Preliminary calibration of a generic scramjet combustor
- Author: P. A. Jacobs
- Number of Pages: Median: 28
- Publisher: ➤ Institute for Computer Applications in Science and Engineering
- Publish Date: 1991
- Publish Location: Hampton, Va
“Preliminary calibration of a generic scramjet combustor” Subjects and Themes:
- Subjects: Ramjet engines - Supersonic combustion
Edition Identifiers:
- The Open Library ID: OL19165695M
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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