Explore: Exhaust Nozzles
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Source: The Open Library
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1Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft
By Barbara S. Esker
“Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft” Metadata:
- Title: ➤ Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft
- Author: Barbara S. Esker
- Language: English
- Number of Pages: Median: 10
- Publisher: ➤ For sale by the National Technical Information Service - NASA
- Publish Date: 1990
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft” Subjects and Themes:
- Subjects: ➤ Airplanes - Short take-off and landing aircraft - Nozzles - Jet propulsion - Ramjet engines - Short takeoff aircraft - Vertical landing - Exhaust nozzles - Swivels
Edition Identifiers:
- The Open Library ID: OL17630526M - OL17726031M
- Online Computer Library Center (OCLC) ID: 24990569
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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2Pitot-pressure measurements in flow fields behind a rectangular nozzle with exhaust jet for free-stream mach numbers of 0.00, 0,60, and 1.20
By Lawrence E. Putnam
“Pitot-pressure measurements in flow fields behind a rectangular nozzle with exhaust jet for free-stream mach numbers of 0.00, 0,60, and 1.20” Metadata:
- Title: ➤ Pitot-pressure measurements in flow fields behind a rectangular nozzle with exhaust jet for free-stream mach numbers of 0.00, 0,60, and 1.20
- Author: Lawrence E. Putnam
- Language: English
- Number of Pages: Median: 151
- Publisher: ➤ National Technical Information Service, distributor] - Langley Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1986
- Publish Location: ➤ [Washington, DC] - [Springfield, Va - Hampton, Va
“Pitot-pressure measurements in flow fields behind a rectangular nozzle with exhaust jet for free-stream mach numbers of 0.00, 0,60, and 1.20” Subjects and Themes:
- Subjects: ➤ Exhaust nozzles - Flow distribution - Free flow - Jet exhaust - Mach number - Nozzles - Pitot tubes - Pressure measurement - Transonic speed
Edition Identifiers:
- The Open Library ID: OL20985250M - OL18083203M - OL15417483M
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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3Ultra-high bypass ratio jet noise
By Low, John, K. C.
“Ultra-high bypass ratio jet noise” Metadata:
- Title: ➤ Ultra-high bypass ratio jet noise
- Author: Low, John, K. C.
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Ultra-high bypass ratio jet noise” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Exhaust nozzles - Wind tunnel tests - Nozzle geometry - Subsonic speed - Bypass ratio - Noise intensity - Noise prediction (Aircraft) - Noise reduction - Jet aircraft noise
Edition Identifiers:
- The Open Library ID: OL17683438M - OL17005197M - OL18078597M
- Online Computer Library Center (OCLC) ID: 32662654
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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4Experimental and analytical studies of flow through a ventral and axial exhaust nozzle system for STOVL aircraft
By Barbara S. Esker
“Experimental and analytical studies of flow through a ventral and axial exhaust nozzle system for STOVL aircraft” Metadata:
- Title: ➤ Experimental and analytical studies of flow through a ventral and axial exhaust nozzle system for STOVL aircraft
- Author: Barbara S. Esker
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1991
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Experimental and analytical studies of flow through a ventral and axial exhaust nozzle system for STOVL aircraft” Subjects and Themes:
- Subjects: ➤ Discharge coefficient - Exhaust nozzles - Nozzle flow - STOVL aircraft - Exhaust systems - Propulsion system performance - Nozzle thrust coefficients
Edition Identifiers:
- The Open Library ID: OL18077140M - OL17683086M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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5Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control
By Scott C. Asbury
“Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control” Metadata:
- Title: ➤ Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control
- Author: Scott C. Asbury
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1999
- Publish Location: Hampton, Va - [Springfield, Va
“Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control” Subjects and Themes:
- Subjects: Cavities - Exhaust nozzles - Hole geometry (Mechanics) - Porosity - Thrust vector control
Edition Identifiers:
- The Open Library ID: OL17592116M - OL15559342M
- Online Computer Library Center (OCLC) ID: 43263577
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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6Experimental and analytical study of close-coupled ventral nozzles for ASTOVL aircraft
By Jack G. McArdle
“Experimental and analytical study of close-coupled ventral nozzles for ASTOVL aircraft” Metadata:
- Title: ➤ Experimental and analytical study of close-coupled ventral nozzles for ASTOVL aircraft
- Author: Jack G. McArdle
- Language: English
- Number of Pages: Median: 14
- Publisher: ➤ National Aeronautics and Space Administration - For sale by the National Technical Information Service
- Publish Date: 1990
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Experimental and analytical study of close-coupled ventral nozzles for ASTOVL aircraft” Subjects and Themes:
- Subjects: ➤ Jet propulsion - Short take-off and landing aircraft - Computational fluid dynamics - Exhaust nozzles - V/STOL aircraft - Flow deflection - Flow distribution - Ducts - Nozzle efficiency - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL17725707M - OL17634488M
- Online Computer Library Center (OCLC) ID: 25003075
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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7Experimental and computational investigation of a translating-throat, single-expansion-ramp nozzle
By Karen A. Deere
“Experimental and computational investigation of a translating-throat, single-expansion-ramp nozzle” Metadata:
- Title: ➤ Experimental and computational investigation of a translating-throat, single-expansion-ramp nozzle
- Author: Karen A. Deere
- 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
“Experimental and computational investigation of a translating-throat, single-expansion-ramp nozzle” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Nozzle efficiency - Exhaust nozzles - K-epsilon turbulence model - Nozzle design - Throats - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL17591581M - OL15557863M
- Online Computer Library Center (OCLC) ID: 42880092
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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8Start up research effort in fluid mechanics
By Samuel G. White
“Start up research effort in fluid mechanics” Metadata:
- Title: ➤ Start up research effort in fluid mechanics
- Author: Samuel G. White
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Start up research effort in fluid mechanics” Subjects and Themes:
- Subjects: Screws - Effectiveness - Jet exhaust - Noise reduction - Exhaust nozzles
Edition Identifiers:
- The Open Library ID: OL15479198M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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9High speed nozzles task
By A. Hamed
“High speed nozzles task” Metadata:
- Title: High speed nozzles task
- Author: A. Hamed
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - University of Cincinnati - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Cincinnati, Ohio?] - [Washington, DC
“High speed nozzles task” Subjects and Themes:
- Subjects: ➤ Convergent-divergent nozzles - Exhaust nozzles - Nozzle design - Nozzle flow - Pressure ratio - Supersonic speed - Turbulence models
Edition Identifiers:
- The Open Library ID: OL15418953M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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10Shelf life extension for the lot AAE nozzle severance LSCs
By M. Cook
“Shelf life extension for the lot AAE nozzle severance LSCs” Metadata:
- Title: ➤ Shelf life extension for the lot AAE nozzle severance LSCs
- Author: M. Cook
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, George C. Marshall Space Flight Center? - Thiokol Corp., Space Operations
- Publish Date: 1990
- Publish Location: ➤ Brigham City, UT - [Marshall Space Flight Center, Ala
“Shelf life extension for the lot AAE nozzle severance LSCs” Subjects and Themes:
- Subjects: Exhaust nozzles - Rocket nozzles - Shaped charges - Solid propellant rocket engines - Storage stability
Edition Identifiers:
- The Open Library ID: OL16138451M
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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11Separate flow nozzle test status meeting
“Separate flow nozzle test status meeting” Metadata:
- Title: ➤ Separate flow nozzle test status meeting
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 2000
- Publish Location: [Washington, DC] - Hanover, MD
“Separate flow nozzle test status meeting” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Sonic nozzles - Exhaust nozzles - Engine noise - Jet aircraft noise - Acoustic nozzles
Edition Identifiers:
- The Open Library ID: OL14524905M
- Online Computer Library Center (OCLC) ID: 50769127
Access and General Info:
- First Year Published: 2000
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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12Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet
By Michael K. Ponton
“Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet” Metadata:
- Title: ➤ Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet
- Author: Michael K. Ponton
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: Hampton, Va - [Springfield, Va
“Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet” Subjects and Themes:
- Subjects: ➤ Exhaust gases - Aeroacoustics - Exhaust nozzles - Jet flow - Flow characteristics - Subsonic flow - Convergent nozzles - High Reynolds number - Engine noise - Pressure oscillations
Edition Identifiers:
- The Open Library ID: OL15550628M
Author's Alternative Names:
"Nichael K. Ponton"Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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13Radiant energy measurements from a scaled jet engine axisymmetric exhaust nozzle for a baseline code validation case
By Joseph F. Baumeister
“Radiant energy measurements from a scaled jet engine axisymmetric exhaust nozzle for a baseline code validation case” Metadata:
- Title: ➤ Radiant energy measurements from a scaled jet engine axisymmetric exhaust nozzle for a baseline code validation case
- Author: Joseph F. Baumeister
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Radiant energy measurements from a scaled jet engine axisymmetric exhaust nozzle for a baseline code validation case” Subjects and Themes:
- Subjects: ➤ Jet engines - Exhaust nozzles - Computer programs - Thermal analysis - Nozzle geometry - Radiation measurement - Aircraft engines
Edition Identifiers:
- The Open Library ID: OL15403957M
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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14A comparison of three Navier-Stokes solvers for exhaust nozzle flowfields
By Nicholas J. Georgiadis
“A comparison of three Navier-Stokes solvers for exhaust nozzle flowfields” Metadata:
- Title: ➤ A comparison of three Navier-Stokes solvers for exhaust nozzle flowfields
- Author: Nicholas J. Georgiadis
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 1999
- Publish Location: ➤ [Springfield, Va - [Cleveland, Ohio]
“A comparison of three Navier-Stokes solvers for exhaust nozzle flowfields” Subjects and Themes:
- Subjects: ➤ Exhaust nozzles - Computational grids - Nozzle flow - Flow characteristics - Ejectors - Turbulent mixing - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL15552382M
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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15An experimental comparison of nonswirling and swirling flow in a circular-to-rectangular transition duct
By Bruce A. Reichert
“An experimental comparison of nonswirling and swirling flow in a circular-to-rectangular transition duct” Metadata:
- Title: ➤ An experimental comparison of nonswirling and swirling flow in a circular-to-rectangular transition duct
- Author: Bruce A. Reichert
- Language: English
- Publisher: Lewis Research Center
- Publish Date: 1991
- Publish Location: [Cleveland, Ohio
“An experimental comparison of nonswirling and swirling flow in a circular-to-rectangular transition duct” Subjects and Themes:
- Subjects: ➤ Ducts - Swirling - Flow geometry - Exhaust nozzles - Nozzle geometry - Ducted flow
Edition Identifiers:
- The Open Library ID: OL16126995M
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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16Internal performance of a fixed-shroud nonaxisymmetric nozzle equipped with an aft-hood exhaust deflector
By Scott C. Asbury
“Internal performance of a fixed-shroud nonaxisymmetric nozzle equipped with an aft-hood exhaust deflector” Metadata:
- Title: ➤ Internal performance of a fixed-shroud nonaxisymmetric nozzle equipped with an aft-hood exhaust deflector
- Author: Scott C. Asbury
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1997
- Publish Location: Hampton, Va - Springfield, VA
“Internal performance of a fixed-shroud nonaxisymmetric nozzle equipped with an aft-hood exhaust deflector” Subjects and Themes:
- Subjects: Wind tunnel tests - Deflectors - Exhaust nozzles
Edition Identifiers:
- The Open Library ID: OL15546765M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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17Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept
By David J. Wing
“Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept” Metadata:
- Title: ➤ Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept
- Author: David J. Wing
- 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
“Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept” Subjects and Themes:
- Subjects: ➤ Testing - Sonic nozzles - Exhaust nozzles - Jet nozzles - Wind tunnel tests - Nozzle geometry - Static tests - Throats - Skewness - Thrust vector control
Edition Identifiers:
- The Open Library ID: OL17000202M
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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18Analysis and design of optimized truncated scarfed nozzles subject to external flow effects
By Rickey J. Shyne
“Analysis and design of optimized truncated scarfed nozzles subject to external flow effects” Metadata:
- Title: ➤ Analysis and design of optimized truncated scarfed nozzles subject to external flow effects
- Author: Rickey J. Shyne
- Language: English
- Number of Pages: Median: 10
- Publisher: ➤ National Aeronautics and Space Administration - For sale by the National Technical Information Service
- Publish Date: 1990
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Analysis and design of optimized truncated scarfed nozzles subject to external flow effects” Subjects and Themes:
- Subjects: ➤ Nozzles - Nozzle design - Ramjet engines - Exhaust nozzles - Nozzle geometry - Airplanes - Flow distribution
Edition Identifiers:
- The Open Library ID: OL16132137M
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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19Titanium aluminide applications in the high speed civil transport
By Paul A. Bartolotta
“Titanium aluminide applications in the high speed civil transport” Metadata:
- Title: ➤ Titanium aluminide applications in the high speed civil transport
- Author: Paul A. Bartolotta
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 1999
- Publish Location: ➤ [Cleveland, Ohio] - Springfield, VA
“Titanium aluminide applications in the high speed civil transport” Subjects and Themes:
- Subjects: Titanium aluminides - Weight reduction - Exhaust nozzles - Noise reduction - Supersonic commercial air transport
Edition Identifiers:
- The Open Library ID: OL15550597M
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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20Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility
By Kin C. Wong
“Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility” Metadata:
- Title: ➤ Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility
- Author: Kin C. Wong
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - Available from the NASA Center for Aerospace Information
- Publish Date: 2003
- Publish Location: ➤ [Cleveland, Ohio] - [Hanover, Md
“Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility” Subjects and Themes:
- Subjects: ➤ Test facilities - Thrust measurement - Exhaust nozzles - Calibrating - Nozzle geometry - Data reduction - Axial loads
Edition Identifiers:
- The Open Library ID: OL16098340M
Access and General Info:
- First Year Published: 2003
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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21Separate flow nozzle test status meeting
“Separate flow nozzle test status meeting” Metadata:
- Title: ➤ Separate flow nozzle test status meeting
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 2000
- Publish Location: [Washington, DC] - Hanover, MD
“Separate flow nozzle test status meeting” Subjects and Themes:
- Subjects: ➤ Jet aircraft noise - Engine noise - Acoustic nozzles - Aeroacoustics - Sonic nozzles - Exhaust nozzles
Edition Identifiers:
- The Open Library ID: OL17607436M
- Online Computer Library Center (OCLC) ID: 50769127
Access and General Info:
- First Year Published: 2000
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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22Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application
By Jagdish S. Sokhey
“Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application” Metadata:
- Title: ➤ Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application
- Author: Jagdish S. Sokhey
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - [Cleveland, Ohio]
“Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application” Subjects and Themes:
- Subjects: ➤ Viscous flow - Powered lift aircraft - Vertical landing - Thrust vector control - Exhaust nozzles - Nozzle flow - Analysis (Mathematics)
Edition Identifiers:
- The Open Library ID: OL15539894M
- Online Computer Library Center (OCLC) ID: 40763709
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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