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Source: The Open Library
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1Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation
By Lawrence D. Huebner
“Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation” Metadata:
- Title: ➤ Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation
- Author: Lawrence D. Huebner
- Language: English
- Number of Pages: Median: 46
- Publisher: ➤ National Technical Information Service, distributor] - Langley Research Center - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1993
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, DC]
“Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation” Subjects and Themes:
- Subjects: Aerodynamics, Hypersonic - Hypersonic Aerodynamics - Hypersonic wind tunnels - Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL15381994M - OL14697258M - OL18062876M - OL20272564M - OL17109819M
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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2Air-breathing aerospace plane development essential
By Unmeel B. Mehta
“Air-breathing aerospace plane development essential” Metadata:
- Title: ➤ Air-breathing aerospace plane development essential
- Author: Unmeel B. Mehta
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Air-breathing aerospace plane development essential” Subjects and Themes:
- Subjects: Aerospace planes - Flight tests - Hypersonic flight - Space transportation - Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL17114622M - OL18078631M - OL16982812M - OL15408586M
- Online Computer Library Center (OCLC) ID: 32668817
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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3A two-line absorption instrument for scramjet temperature and water vapor concentration measurement in HYPULSE
By C. Y. Tsai
“A two-line absorption instrument for scramjet temperature and water vapor concentration measurement in HYPULSE” Metadata:
- Title: ➤ A two-line absorption instrument for scramjet temperature and water vapor concentration measurement in HYPULSE
- Author: C. Y. Tsai
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1998
- Publish Location: Hampton, Va - [Springfield, Va
“A two-line absorption instrument for scramjet temperature and water vapor concentration measurement in HYPULSE” Subjects and Themes:
- Subjects: ➤ Temperature measurement - Supersonic combustion ramjet engines - Combustion chambers - Calibrating
Edition Identifiers:
- The Open Library ID: OL17583582M - OL18134687M - OL15547826M - OL17133665M
- Online Computer Library Center (OCLC) ID: 42212554
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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4Shock-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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5High-speed engine/component performance assessment using exergy and thrust-based methods
By D. W. Riggins
“High-speed engine/component performance assessment using exergy and thrust-based methods” Metadata:
- Title: ➤ High-speed engine/component performance assessment using exergy and thrust-based methods
- Author: D. W. Riggins
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: [Springfield, Va - Hampton, Va
“High-speed engine/component performance assessment using exergy and thrust-based methods” Subjects and Themes:
- Subjects: ➤ Brayton cycle - Engine parts - Engine tests - Performance tests - Supersonic combustion ramjet engines - Thrust
Edition Identifiers:
- The Open Library ID: OL18086871M - OL17107861M - OL15423143M
- Online Computer Library Center (OCLC) ID: 35252174
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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6Viscous computations of cold air/airflow around scramjet nozzle afterbody
By Oktay Baysal
“Viscous computations of cold air/airflow around scramjet nozzle afterbody” Metadata:
- Title: ➤ Viscous computations of cold air/airflow around scramjet nozzle afterbody
- Author: Oktay Baysal
- Language: English
- Number of Pages: Median: 65
- Publisher: ➤ For sale by the National Technical Information Service] - Langley Research Center - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1991
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, DC]
“Viscous computations of cold air/airflow around scramjet nozzle afterbody” Subjects and Themes:
- Subjects: Computational fluid dynamics - Hypersonic Aerodynamics - Hypersonic vehicles - Jet nozzles - Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL15372804M - OL21499696M
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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7Hypersonic combined cycle propulsion
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
“Hypersonic combined cycle propulsion” Metadata:
- Title: ➤ Hypersonic combined cycle propulsion
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
- Number of Pages: Median: 472
- Publisher: AGARD
- Publish Date: 1990
- Publish Location: Neuilly sur Seine, France
“Hypersonic combined cycle propulsion” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL19165500M - OL19165597M
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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8A 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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9Numerical study of hydrogen-air supersonic combustion by using elliptic and parabolized equations
By Tawit Chitsomboon
“Numerical study of hydrogen-air supersonic combustion by using elliptic and parabolized equations” Metadata:
- Title: ➤ Numerical study of hydrogen-air supersonic combustion by using elliptic and parabolized equations
- Author: Tawit Chitsomboon
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - Dept. of Chemical Sciences, College of Sciences, Old Dominion University
- Publish Date: 1986
- Publish Location: ➤ Norfolk, Va - [Washington, DC - Springfield, Va
“Numerical study of hydrogen-air supersonic combustion by using elliptic and parabolized equations” Subjects and Themes:
- Subjects: ➤ Applications programs (Computers) - Chemical reactions - Continuity (Mathematics) - Navier-Stokes equations - Numerical analysis - Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL17684188M - OL14984836M
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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10Mach 10 experimental database of a three-dimensional scramjet inlet flow field
By Scott D. Holland
“Mach 10 experimental database of a three-dimensional scramjet inlet flow field” Metadata:
- Title: ➤ Mach 10 experimental database of a three-dimensional scramjet inlet flow field
- Author: Scott D. Holland
- Language: English
- Number of Pages: Median: 214
- Publisher: ➤ Available from the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1995
- Publish Location: ➤ Hampton, Va - [Springfield, VA - Springfield, VA
“Mach 10 experimental database of a three-dimensional scramjet inlet flow field” Subjects and Themes:
- Subjects: ➤ Aerodynamics, Hypersonic - Air intakes - Airplanes - Computational fluid dynamics - Engine inlets - Flow distribution - Hypersonic Aerodynamics - Hypersonic speed - Inlet flow - Internal flow - Laminar boundary layer - Oblique shock waves - Pressure measurement - Ramjet engines - Scramjet engines - Shock wave interaction - Supersonic combustion ramjet engines - Three dimensional flow - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL16125691M - OL17141237M
- Online Computer Library Center (OCLC) ID: 33230284
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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11Instrumentation 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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12Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6
By Scott Douglas Holland
“Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6” Metadata:
- Title: ➤ Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6
- Author: Scott Douglas Holland
- 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
“Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6” Subjects and Themes:
- Subjects: ➤ Inlet flow - Actuators - Hypersonic wind tunnels - Supersonic combustion ramjet engines - Blocking - Engine inlets - Hypersonic inlets - Cowlings - Wind tunnel tests - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15409524M - OL18079126M
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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13Recent 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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14Investigation of ramp injectors for supersonic mixing enhancement
By Y. Haimovitch
“Investigation of ramp injectors for supersonic mixing enhancement” Metadata:
- Title: ➤ Investigation of ramp injectors for supersonic mixing enhancement
- Author: Y. Haimovitch
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1994
- Publish Location: [Springfield, VA - Hampton, Va
“Investigation of ramp injectors for supersonic mixing enhancement” Subjects and Themes:
- Subjects: ➤ Nozzle inserts - Fuel injection - Supersonic flow - Nozzle geometry - Supersonic combustion ramjet engines - Turbulent mixing - Spray nozzles - Wind tunnel tests - Injectors
Edition Identifiers:
- The Open Library ID: OL15409145M - OL17790638M
- Online Computer Library Center (OCLC) ID: 32712612
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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15Advances in hypersonic vehicle synthesis with application to studies of advanced thermal protection systems
final report
By Mark D. Ardema
“Advances in hypersonic vehicle synthesis with application to studies of advanced thermal protection systems” Metadata:
- Title: ➤ Advances in hypersonic vehicle synthesis with application to studies of advanced thermal protection systems
- Author: Mark D. Ardema
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Advances in hypersonic vehicle synthesis with application to studies of advanced thermal protection systems” Subjects and Themes:
- Subjects: ➤ Thermal protection - Engine design - Single stage to orbit vehicles - Trajectory optimization - Hypersonic vehicles - Supersonic combustion ramjet engines - Propulsion system configurations
Edition Identifiers:
- The Open Library ID: OL17793601M - OL15419795M
- Online Computer Library Center (OCLC) ID: 34696123
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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16Studies in scramjet flowfields
By Joseph A. Schetz
“Studies in scramjet flowfields” Metadata:
- Title: Studies in scramjet flowfields
- Author: Joseph A. Schetz
- Number of Pages: Median: 15
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1987
- Publish Location: [S.l.]
“Studies in scramjet flowfields” Subjects and Themes:
- Subjects: ➤ Flow distribution - Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL19005649M
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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17Heat pipe cooling for scramjet engines
By Calvin C. Silverstein
“Heat pipe cooling for scramjet engines” Metadata:
- Title: ➤ Heat pipe cooling for scramjet engines
- Author: Calvin C. Silverstein
- Language: English
- Publisher: ➤ National Technical Information Service, distributor] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1986
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Heat pipe cooling for scramjet engines” Subjects and Themes:
- Subjects: Cooling - Heat pipes - Linings - Liquid metals - Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL17684211M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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18Shock tunnel studies of scramjet phenomena
“Shock tunnel studies of scramjet phenomena” Metadata:
- Title: ➤ Shock tunnel studies of scramjet phenomena
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Shock tunnel studies of scramjet phenomena” Subjects and Themes:
- Subjects: ➤ Shock tunnels - Supersonic combustion ramjet engines - Data acquisition - Enthalpy - Investigation - Thrust - Hypersonic nozzles - Mach number
Edition Identifiers:
- The Open Library ID: OL17837869M
- Online Computer Library Center (OCLC) ID: 40691816
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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19Experimental determination of hydrogen-air detonation pressure limit and scramjet application
By R. Skyring
“Experimental determination of hydrogen-air detonation pressure limit and scramjet application” Metadata:
- Title: ➤ Experimental determination of hydrogen-air detonation pressure limit and scramjet application
- Author: R. Skyring
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1996
- Publish Location: Washington
“Experimental determination of hydrogen-air detonation pressure limit and scramjet application” Subjects and Themes:
- Subjects: ➤ Supersonic combustion ramjet engines - Detonation waves
Edition Identifiers:
- The Open Library ID: OL22347293M
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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20Hydrogen 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
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21Computational models for the analysis/design of hypersonic scramjet nozzles - Part 1
By Sanford M. Dash
“Computational models for the analysis/design of hypersonic scramjet nozzles - Part 1” Metadata:
- Title: ➤ Computational models for the analysis/design of hypersonic scramjet nozzles - Part 1
- Author: Sanford M. Dash
- Number of Pages: Median: 19
- Publisher: AIAA
- Publish Date: 1986
- Publish Location: New York
“Computational models for the analysis/design of hypersonic scramjet nozzles - Part 1” Subjects and Themes:
- Subjects: ➤ Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL20985290M
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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22A mixing augmentation technique for hypervelocity scramjets
By Ajay Kumar
“A mixing augmentation technique for hypervelocity scramjets” Metadata:
- Title: ➤ A mixing augmentation technique for hypervelocity scramjets
- Author: Ajay Kumar
- Number of Pages: Median: 15
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1987
- Publish Location: Washington
“A mixing augmentation technique for hypervelocity scramjets” Subjects and Themes:
- Subjects: ➤ Mixing - Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL19246182M
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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23User's guide for NASCRIN - a vectorized code for calculating two-dimensional supersonic internal flow fields
By Ajay Kumar
“User's guide for NASCRIN - a vectorized code for calculating two-dimensional supersonic internal flow fields” Metadata:
- Title: ➤ User's guide for NASCRIN - a vectorized code for calculating two-dimensional supersonic internal flow fields
- Author: Ajay Kumar
- Number of Pages: Median: 67
- Publisher: Langley Research Center
- Publish Date: 1984
- Publish Location: Hampton, Va
“User's guide for NASCRIN - a vectorized code for calculating two-dimensional supersonic internal flow fields” Subjects and Themes:
- Subjects: ➤ Euler equations of motion - Inlet flow - Supersonic combustion ramjet engines - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL20986766M
Access and General Info:
- First Year Published: 1984
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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24Research in robust control for hypersonic vehicles
By Anthony J. Calise
“Research in robust control for hypersonic vehicles” Metadata:
- Title: ➤ Research in robust control for hypersonic vehicles
- Author: Anthony J. Calise
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - School of Aerospace Engineering, Georgia Institute of Technology
- Publish Date: 1992
- Publish Location: ➤ Springfield, Va - Atlanta, Ga - [Washington, DC
“Research in robust control for hypersonic vehicles” Subjects and Themes:
- Subjects: ➤ Flight control - Engine design - Dynamic models - Hypersonic vehicles - Supersonic combustion ramjet engines - Mach number - Angle of attack
Edition Identifiers:
- The Open Library ID: OL15404655M
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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25Schlieren photographs and internal pressure distributions for three-dimensional sidewall-compression scramjet inlets at a Mach number of 6 in CF4
By Scott D. Holland
“Schlieren photographs and internal pressure distributions for three-dimensional sidewall-compression scramjet inlets at a Mach number of 6 in CF4” Metadata:
- Title: ➤ Schlieren photographs and internal pressure distributions for three-dimensional sidewall-compression scramjet inlets at a Mach number of 6 in CF4
- Author: Scott D. Holland
- Number of Pages: Median: 140
- Publisher: Langley Research Center
- Publish Date: 1993
- Publish Location: Hampton, Va
“Schlieren photographs and internal pressure distributions for three-dimensional sidewall-compression scramjet inlets at a Mach number of 6 in CF4” Subjects and Themes:
- Subjects: ➤ Supersonic combustion ramjet engines - Inlets
Edition Identifiers:
- The Open Library ID: OL19916624M
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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26Reduced H2-O2 mechanisms for use in reacting flow simulation
By B. D. Hitch
“Reduced H2-O2 mechanisms for use in reacting flow simulation” Metadata:
- Title: ➤ Reduced H2-O2 mechanisms for use in reacting flow simulation
- Author: B. D. Hitch
- Number of Pages: Median: 10
- Publisher: AIAA
- Publish Date: 1988
- Publish Location: New York
“Reduced H2-O2 mechanisms for use in reacting flow simulation” Subjects and Themes:
- Subjects: ➤ Hydrogen oxygen engines - Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL18926367M
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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27Calculated chemical and vibrational nonequilibrium effects in NASP-type nozzles
By Oussama F. Rizkalla
“Calculated chemical and vibrational nonequilibrium effects in NASP-type nozzles” Metadata:
- Title: ➤ Calculated chemical and vibrational nonequilibrium effects in NASP-type nozzles
- Author: Oussama F. Rizkalla
- Number of Pages: Median: 11
- Publisher: AIAA
- Publish Date: 1988
- Publish Location: New York
“Calculated chemical and vibrational nonequilibrium effects in NASP-type nozzles” Subjects and Themes:
- Subjects: ➤ Nozzles - Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL18927714M
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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28Scramjet nozzle analysis
By Sanford S. Hammer
“Scramjet nozzle analysis” Metadata:
- Title: Scramjet nozzle analysis
- Author: Sanford S. Hammer
- Number of Pages: Median: 74
- Publisher: Propulsion Sciences, Inc
- Publish Date: 1970
- Publish Location: Melville, N.Y
“Scramjet nozzle analysis” Subjects and Themes:
- Subjects: ➤ Nozzles - Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL18931043M
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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29Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6
By Scott D. Holland
“Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6” Metadata:
- Title: ➤ Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6
- Author: Scott D. Holland
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: [Springfield, Va - Hampton, Va
“Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6” Subjects and Themes:
- Subjects: ➤ Inlet flow - Actuators - Hypersonic wind tunnels - Supersonic combustion ramjet engines - Blocking - Engine inlets - Hypersonic inlets - Cowlings - Wind tunnel tests - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL17114738M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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30Turbulent transport models for scramjet flowfields
By M. M. Sindir
“Turbulent transport models for scramjet flowfields” Metadata:
- Title: ➤ Turbulent transport models for scramjet flowfields
- Author: M. M. Sindir
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1984
- Publish Location: Hampton, Va
“Turbulent transport models for scramjet flowfields” Subjects and Themes:
- Subjects: ➤ Unsteady flow (Aerodynamics) - Transport properties - Turbulence - Turbulence models - Supersonic combustion ramjet engines - Turbulent mixing - Flow distribution
Edition Identifiers:
- The Open Library ID: OL16156989M
Access and General Info:
- First Year Published: 1984
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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31Parametric studies of the ejector process within a turbine-based combined-cycle propulsion system
By Nicholas J. Georgiadis
“Parametric studies of the ejector process within a turbine-based combined-cycle propulsion system” Metadata:
- Title: ➤ Parametric studies of the ejector process within a turbine-based combined-cycle propulsion system
- 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]
“Parametric studies of the ejector process within a turbine-based combined-cycle propulsion system” Subjects and Themes:
- Subjects: ➤ Aircraft configurations - Computational fluid dynamics - Ejectors - K-epsilon turbulence model - Multigrid methods - Navier-Stokes equation - Propulsion system configurations - Propulsion system performance - Ramjet engines - Supersonic combustion ramjet engines - Turbulent mixing - Two dimensional flow
Edition Identifiers:
- The Open Library ID: OL15550614M
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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32Optimized scramjet integration on a waverider
By Mary Kae L. O'Neill
“Optimized scramjet integration on a waverider” Metadata:
- Title: ➤ Optimized scramjet integration on a waverider
- Author: Mary Kae L. O'Neill
- Number of Pages: Median: 12
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1991
- Publish Location: Washington, D. C
“Optimized scramjet integration on a waverider” Subjects and Themes:
- Subjects: ➤ Waveriders - Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL19245454M
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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33Investigation of a 2-D scramjet inlet, M =8-25 and T =800-4, 100K
By Marco A. S. Minucci
“Investigation of a 2-D scramjet inlet, M =8-25 and T =800-4, 100K” Metadata:
- Title: ➤ Investigation of a 2-D scramjet inlet, M =8-25 and T =800-4, 100K
- Author: Marco A. S. Minucci
- Number of Pages: Median: 18
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1991
- Publish Location: Washington, D. C
“Investigation of a 2-D scramjet inlet, M =8-25 and T =800-4, 100K” Subjects and Themes:
- Subjects: ➤ Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL19245519M
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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34Scramjet testing from Mach 4 to 20
By Scott R. Thomas
“Scramjet testing from Mach 4 to 20” Metadata:
- Title: ➤ Scramjet testing from Mach 4 to 20
- Author: Scott R. Thomas
- Number of Pages: Median: 27
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1990
- Publish Location: Washington, D. C
“Scramjet testing from Mach 4 to 20” Subjects and Themes:
- Subjects: ➤ Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL21379246M
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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35Numerical study of supersonic combustors by multi-block grids with mismatched interfaces
By Young J. Moon
“Numerical study of supersonic combustors by multi-block grids with mismatched interfaces” Metadata:
- Title: ➤ Numerical study of supersonic combustors by multi-block grids with mismatched interfaces
- Author: Young J. Moon
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1990
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Numerical study of supersonic combustors by multi-block grids with mismatched interfaces” Subjects and Themes:
- Subjects: ➤ Computerized simulation - Computational grids - Combustion chambers - Three dimensional flow - Supersonic combustion ramjet engines - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL15405893M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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36Further shock tunnel studies of scramjet phenomena
By R. G. Morgan
“Further shock tunnel studies of scramjet phenomena” Metadata:
- Title: ➤ Further shock tunnel studies of scramjet phenomena
- Author: R. G. Morgan
- Number of Pages: Median: 57
- Publisher: University of Queensland
- Publish Date: 1986
- Publish Location: St.Lucia, Australia
“Further shock tunnel studies of scramjet phenomena” Subjects and Themes:
- Subjects: ➤ Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL18999368M
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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37Scramjet mixing establishment times for a pulse facility
By R. Clayton Rogers
“Scramjet mixing establishment times for a pulse facility” Metadata:
- Title: ➤ Scramjet mixing establishment times for a pulse facility
- Author: R. Clayton Rogers
- Number of Pages: Median: 14
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1991
- Publish Location: Washington, D. C
“Scramjet mixing establishment times for a pulse facility” Subjects and Themes:
- Subjects: ➤ Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL21499550M
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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38Human exploration and settlement of the moon using LUNOX-augmented NTR propulsion
By Stanley K. Borowski
“Human exploration and settlement of the moon using LUNOX-augmented NTR propulsion” Metadata:
- Title: ➤ Human exploration and settlement of the moon using LUNOX-augmented NTR propulsion
- Author: Stanley K. Borowski
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Human exploration and settlement of the moon using LUNOX-augmented NTR propulsion” Subjects and Themes:
- Subjects: ➤ Brayton cycle - Liquid rocket propellants - Low earth orbits - Lunar orbits - Moon - Nuclear rocket engines - Propulsion - Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL15420768M
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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39Mixing enhancement of reacting parallel fuel jets in a supersonic combustor
By J. Philip Drummond
“Mixing enhancement of reacting parallel fuel jets in a supersonic combustor” Metadata:
- Title: ➤ Mixing enhancement of reacting parallel fuel jets in a supersonic combustor
- Author: J. Philip Drummond
- Number of Pages: Median: 14
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1991
- Publish Location: Washington, D. C
“Mixing enhancement of reacting parallel fuel jets in a supersonic combustor” Subjects and Themes:
- Subjects: ➤ Mixing - Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL19752283M
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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40Supersonic 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
Online Access
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41An investigation of a contoured wall injector for hypervelocity mixing augmentation
By Ian A. Waitz
“An investigation of a contoured wall injector for hypervelocity mixing augmentation” Metadata:
- Title: ➤ An investigation of a contoured wall injector for hypervelocity mixing augmentation
- Author: Ian A. Waitz
- Number of Pages: Median: 18
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1991
- Publish Location: Washington, D. C
“An investigation of a contoured wall injector for hypervelocity mixing augmentation” Subjects and Themes:
- Subjects: ➤ Mixing - Fuel injection - Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL19752287M
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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42Supersonic combustion ramjet research at Langley
By G. Burton Northam
“Supersonic combustion ramjet research at Langley” Metadata:
- Title: ➤ Supersonic combustion ramjet research at Langley
- Author: G. Burton Northam
- Number of Pages: Median: 17
- Publisher: AIAA
- Publish Date: 1986
- Publish Location: New York
“Supersonic combustion ramjet research at Langley” Subjects and Themes:
- Subjects: ➤ Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL20984271M
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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43Shock-wave-induced mixing enhancement in scramjet combustors
By S. Menon
“Shock-wave-induced mixing enhancement in scramjet combustors” Metadata:
- Title: ➤ Shock-wave-induced mixing enhancement in scramjet combustors
- Author: S. Menon
- Number of Pages: Median: 15
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1989
- Publish Location: Washington, D. C
“Shock-wave-induced mixing enhancement in scramjet combustors” Subjects and Themes:
- Subjects: ➤ Mixing - Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL19752297M
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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44A numerical and experimental study of a supersonic combustor employing swept ramp fuel injectors
By Dean R. Eklund
“A numerical and experimental study of a supersonic combustor employing swept ramp fuel injectors” Metadata:
- Title: ➤ A numerical and experimental study of a supersonic combustor employing swept ramp fuel injectors
- Author: Dean R. Eklund
- Number of Pages: Median: 20
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1994
- Publish Location: Washington, D. C
“A numerical and experimental study of a supersonic combustor employing swept ramp fuel injectors” Subjects and Themes:
- Subjects: ➤ Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL19755645M
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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45A computational and experimental investigation of a three-dimensional hypersonic scramjet inlet flow field
By Scott Douglas Holland
“A computational and experimental investigation of a three-dimensional hypersonic scramjet inlet flow field” Metadata:
- Title: ➤ A computational and experimental investigation of a three-dimensional hypersonic scramjet inlet flow field
- Author: Scott Douglas Holland
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - North Carolina State University
- Publish Date: 1991
- Publish Location: ➤ Springfield, Va - Raleligh, NC - [Washington, DC
“A computational and experimental investigation of a three-dimensional hypersonic scramjet inlet flow field” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Inlet flow - Supersonic combustion ramjet engines - Three dimensional flow - Hypersonic inlets - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15405796M
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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46Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10
By Scott Douglas Holland
“Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10” Metadata:
- Title: ➤ Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10
- Author: Scott Douglas Holland
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center - NASA Center for AeroSpace Information, distributor
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - Hampton, Va - Linthicum Heights, MD
“Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10” Subjects and Themes:
- Subjects: ➤ Inlet flow - Engine design - Hypersonic inlets - Wind tunnel tests - Supersonic combustion ramjet engines - Flow distribution - Hypersonic speed - Internal flow - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15412088M
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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47Mach 10 computational study of a three-dimensional scramjet inlet flow field
By Scott Douglas Holland
“Mach 10 computational study of a three-dimensional scramjet inlet flow field” Metadata:
- Title: ➤ Mach 10 computational study of a three-dimensional scramjet inlet flow field
- Author: Scott Douglas Holland
- 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
“Mach 10 computational study of a three-dimensional scramjet inlet flow field” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Inlet flow - Computational grids - Aerodynamics - Three dimensional flow - Supersonic combustion ramjet engines - Navier-Stokes equation - Hypersonic speed - Supersonic inlets - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15410430M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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48Progress toward synergistic hypermixing nozzles
By D. O. Davis
“Progress toward synergistic hypermixing nozzles” Metadata:
- Title: ➤ Progress toward synergistic hypermixing nozzles
- Author: D. O. Davis
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1991
- Publish Location: Washington, D. C
“Progress toward synergistic hypermixing nozzles” Subjects and Themes:
- Subjects: ➤ Mixing - Nozzles - Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL19752256M
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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49NASA's hypersonic research engine project
By Earl H. Andrews
“NASA's hypersonic research engine project” Metadata:
- Title: ➤ NASA's hypersonic research engine project
- Author: Earl H. Andrews
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: [Springfield, Va - Hampton, Va
“NASA's hypersonic research engine project” Subjects and Themes:
- Subjects: ➤ Engine design - Wind tunnel tests - Supersonic combustion ramjet engines - Histories - NASA programs - Engine tests - Aircraft engines - Ground tests - Bibliographies
Edition Identifiers:
- The Open Library ID: OL17113963M
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.
Online Borrowing:
Online Marketplaces
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50Options for flight testing rocket-based combined-cycle (RBCC) engines
By J. Olds
“Options for flight testing rocket-based combined-cycle (RBCC) engines” Metadata:
- Title: ➤ Options for flight testing rocket-based combined-cycle (RBCC) engines
- Author: J. Olds
- Language: English
- Publisher: ➤ American Institute of Aeronautics and Astronautics - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ Reston, VA - [Washington, DC - Springfield, Va
“Options for flight testing rocket-based combined-cycle (RBCC) engines” Subjects and Themes:
- Subjects: ➤ Engine tests - Supersonic combustion ramjet engines - X-34 reusable launch vehicle - Flight tests - Rocket engines
Edition Identifiers:
- The Open Library ID: OL15499063M
Access and General Info:
- First Year Published: 1996
- 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.
Online Borrowing:
Online Marketplaces
Find Options for flight testing rocket-based combined-cycle (RBCC) engines at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.