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Books Results
Source: The Open Library
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Search results from The Open Library
1Flow analysis and design optimization methods for nozzle afterbody of a hypersonic vehicle
By Oktay Baysal
“Flow analysis and design optimization methods for nozzle afterbody of a hypersonic vehicle” Metadata:
- Title: ➤ Flow analysis and design optimization methods for nozzle afterbody of a hypersonic vehicle
- Author: Oktay Baysal
- Language: English
- Number of Pages: Median: 51
- Publisher: ➤ Langley Research Center - National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1992
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, D.C.]
“Flow analysis and design optimization methods for nozzle afterbody of a hypersonic vehicle” Subjects and Themes:
- Subjects: Afterbodies - Hypersonic Aerodynamics - Hypersonic nozzles
Edition Identifiers:
- The Open Library ID: OL19243539M - OL15369734M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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2Validation of the NPARC code for nozzle afterbody flows at transonic speeds
By James R. DeBonis
“Validation of the NPARC code for nozzle afterbody flows at transonic speeds” Metadata:
- Title: ➤ Validation of the NPARC code for nozzle afterbody flows at transonic speeds
- Author: James R. DeBonis
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Validation of the NPARC code for nozzle afterbody flows at transonic speeds” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Applications programs (Computers) - Nozzle flow - Afterbodies - Turbulence models - Program verification (Computers) - Transonic speed
Edition Identifiers:
- The Open Library ID: OL17791907M - OL15414431M
- Online Computer Library Center (OCLC) ID: 34041515
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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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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3Experimental aerothermodynamic research of hypersonic aircraft
By Joseph W. Cleary
“Experimental aerothermodynamic research of hypersonic aircraft” Metadata:
- Title: ➤ Experimental aerothermodynamic research of hypersonic aircraft
- Author: Joseph W. Cleary
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1987 - 1989
- Publish Location: ➤ Springfield, Va.? - [Washington, DC
“Experimental aerothermodynamic research of hypersonic aircraft” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Pressure distribution - Afterbodies - Forebodies - Flow distribution - Aerothermodynamics - Hypersonic aircraft - Wind tunnel models - Aerodynamic configurations
Edition Identifiers:
- The Open Library ID: OL15398951M - OL15408376M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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4Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds
By Jack Nugent
“Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds” Metadata:
- Title: ➤ Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds
- Author: Jack Nugent
- Language: English
- Number of Pages: Median: 120
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - Ames Research Center - For sale by the National Technical Information Service]
- Publish Date: 1987 - 1988
- Publish Location: ➤ Edwards, Calif - [Springfield, Va - [Washington, DC]
“Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds” Subjects and Themes:
- Subjects: Aerodynamics, Transonic - Afterbodies - Nozzle flow - Reynolds number - Transonic Aerodynamics
Edition Identifiers:
- The Open Library ID: OL14662959M - OL18998718M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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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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5Computational design aspects of a NASP nozzle/afterbody experiment
By Stephen M. Ruffin
“Computational design aspects of a NASP nozzle/afterbody experiment” Metadata:
- Title: ➤ Computational design aspects of a NASP nozzle/afterbody experiment
- Author: Stephen M. Ruffin
- Number of Pages: Median: 14
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1989
- Publish Location: Washington, D. C
“Computational design aspects of a NASP nozzle/afterbody experiment” Subjects and Themes:
- Subjects: Afterbodies - Aerospace planes - Nozzle flow
Edition Identifiers:
- The Open Library ID: OL19247133M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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6Transonic Navier-Stokes solutions of three-dimensional afterbody flows
By William B. Compton
“Transonic Navier-Stokes solutions of three-dimensional afterbody flows” Metadata:
- Title: ➤ Transonic Navier-Stokes solutions of three-dimensional afterbody flows
- Author: William B. Compton
- Number of Pages: Median: 58
- Publisher: Langley Research Center
- Publish Date: 1989
- Publish Location: Hampton, Va
“Transonic Navier-Stokes solutions of three-dimensional afterbody flows” Subjects and Themes:
- Subjects: Afterbodies - Navier-Stokes equation - Transonic flow
Edition Identifiers:
- The Open Library ID: OL19379696M
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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7Computational assessment of aft-body closure for the HSR reference H configuration
By W. Kelly Londenberg
“Computational assessment of aft-body closure for the HSR reference H configuration” Metadata:
- Title: ➤ Computational assessment of aft-body closure for the HSR reference H configuration
- Author: W. Kelly Londenberg
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1999
- Publish Location: Hampton, Va - Springfield, VA
“Computational assessment of aft-body closure for the HSR reference H configuration” Subjects and Themes:
- Subjects: Afterbodies - Closures - Aerodynamic configurations
Edition Identifiers:
- The Open Library ID: OL15567864M
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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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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8Interference on a model afterbody from downstream support hardware at transonic Mach numbers
By Earl A. Price
“Interference on a model afterbody from downstream support hardware at transonic Mach numbers” Metadata:
- Title: ➤ Interference on a model afterbody from downstream support hardware at transonic Mach numbers
- Author: Earl A. Price
- Number of Pages: Median: 48
- Publisher: ➤ Arnold Engineering Development Center/DOT, Air Force Systems Command
- Publish Date: 1981
- Publish Location: Arnold Air Force Station, Tenn
“Interference on a model afterbody from downstream support hardware at transonic Mach numbers” Subjects and Themes:
- Subjects: Afterbodies - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL20983821M
Access and General Info:
- First Year Published: 1981
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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9Exhausted plume flow field prediction near the afterbody of hypersonic flight vehicles in high altitudes
By Zheng-Tao Deng
“Exhausted plume flow field prediction near the afterbody of hypersonic flight vehicles in high altitudes” Metadata:
- Title: ➤ Exhausted plume flow field prediction near the afterbody of hypersonic flight vehicles in high altitudes
- Author: Zheng-Tao Deng
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Exhausted plume flow field prediction near the afterbody of hypersonic flight vehicles in high altitudes” Subjects and Themes:
- Subjects: ➤ Computerized simulation - Afterbodies - Flow distribution - High altitude - Burnett equations - Hypersonic flow - Plumes - Grid generation (Mathematics) - Hypersonic vehicles
Edition Identifiers:
- The Open Library ID: OL17834451M
- Online Computer Library Center (OCLC) ID: 39618386
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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10The effect of exhaust plume/afterbody interaction on installed scramjet performance
By Thomas A. Edwards
“The effect of exhaust plume/afterbody interaction on installed scramjet performance” Metadata:
- Title: ➤ The effect of exhaust plume/afterbody interaction on installed scramjet performance
- Author: Thomas A. Edwards
- Language: English
- Number of Pages: Median: 95
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1988
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“The effect of exhaust plume/afterbody interaction on installed scramjet performance” Subjects and Themes:
- Subjects: ➤ Afterbodies - Airplanes - Exhaust gases - Hypersonic Aerodynamics - Hypersonic planes - Installing - Plumes - Scramjet engines - Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL15407170M
Access and General Info:
- First Year Published: 1988
- 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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