Explore: Ejectors
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Source: The Open Library
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1Supersonic ejectors
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
“Supersonic ejectors” Metadata:
- Title: Supersonic ejectors
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
- Language: English
- Number of Pages: Median: 187
- Publisher: AGARD
- Publish Date: 1972
- Publish Location: ➤ [Neuilly-sur-Seine - Neuilly-sur-Seine
“Supersonic ejectors” Subjects and Themes:
- Subjects: ➤ Ejectors - Short take-off and landing aircraft
Edition Identifiers:
- The Open Library ID: OL19354360M - OL19031378M
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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2Use of an approximate similarity principle for the thermal scaling of a full-scale thrust augmenting ejector
By Wendy S. Barankiewicz
“Use of an approximate similarity principle for the thermal scaling of a full-scale thrust augmenting ejector” Metadata:
- Title: ➤ Use of an approximate similarity principle for the thermal scaling of a full-scale thrust augmenting ejector
- Author: Wendy S. Barankiewicz
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration
- Publish Date: 1992
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Use of an approximate similarity principle for the thermal scaling of a full-scale thrust augmenting ejector” Subjects and Themes:
- Subjects: Ejectors - Jet propulsion - Vertically rising aircraft - Short take-off and landing aircraft
Edition Identifiers:
- The Open Library ID: OL17675848M - OL14683208M
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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3A control-volume method for analysis of unsteady thrust augmenting ejector flows
By Colin K. Drummond
“A control-volume method for analysis of unsteady thrust augmenting ejector flows” Metadata:
- Title: ➤ A control-volume method for analysis of unsteady thrust augmenting ejector flows
- Author: Colin K. Drummond
- Language: English
- Publisher: ➤ Lewis Research Center, National Aeronautics and Space Administration - For sale by the National Technical Information Service
- Publish Date: 1988
- Publish Location: ➤ Cleveland, Ohio - [Springfield, Va
“A control-volume method for analysis of unsteady thrust augmenting ejector flows” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Unsteady flow - Computerized simulation - Mathematical models - Finite volume method - Turbulent jets - Thrust augmentation - Ejectors
Edition Identifiers:
- The Open Library ID: OL15407668M - OL18078298M
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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4A model for prediction of STOVL ejector dynamics
By Colin K. Drummond
“A model for prediction of STOVL ejector dynamics” Metadata:
- Title: ➤ A model for prediction of STOVL ejector dynamics
- Author: Colin K. Drummond
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - For sale by the National Technical Information Service
- Publish Date: 1989
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“A model for prediction of STOVL ejector dynamics” Subjects and Themes:
- Subjects: Vertically rising aircraft - Ejectors - Jet propulsion
Edition Identifiers:
- The Open Library ID: OL17100899M - OL17661280M
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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5A modeling technique for STOVL ejector and volume dynamics
By Colin K. Drummond
“A modeling technique for STOVL ejector and volume dynamics” Metadata:
- Title: ➤ A modeling technique for STOVL ejector and volume dynamics
- Author: Colin K. Drummond
- Language: English
- Number of Pages: Median: 11
- Publisher: ➤ NASA - For sale by the National Technical Information Service
- Publish Date: 1990
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“A modeling technique for STOVL ejector and volume dynamics” Subjects and Themes:
- Subjects: ➤ Mathematical models - Jet propulsion - Short take-off and landing aircraft - Ejectors - Computational fluid dynamics - V/STOL aircraft - Aircraft configurations - Performance prediction - Thrust
Edition Identifiers:
- The Open Library ID: OL17634486M - OL16132181M
- Online Computer Library Center (OCLC) ID: 25053445
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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6Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight
By Scott R. Thomas
“Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight” Metadata:
- Title: ➤ Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight
- Author: Scott R. Thomas
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight” Subjects and Themes:
- Subjects: ➤ Hydrocarbon fuels - Supersonic speed - Propulsion system performance - Flow distribution - Engine tests - Integral rocket ramjets - Mach number - Ejectors - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15484276M - OL17822489M
- Online Computer Library Center (OCLC) ID: 38850490
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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7Thrust augmentation measurements using a pulse detonation engine ejector
By Robert J. Santoro
“Thrust augmentation measurements using a pulse detonation engine ejector” Metadata:
- Title: ➤ Thrust augmentation measurements using a pulse detonation engine ejector
- Author: Robert J. Santoro
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - National Technical Information Service [distributor - Available from NASA Center for Aerospace Information
- Publish Date: 2003
- Publish Location: ➤ [Cleveland, Ohio] - Springfield, VA - Hanover, MD
“Thrust augmentation measurements using a pulse detonation engine ejector” Subjects and Themes:
- Subjects: Thrust measurement - Ejectors - Pulse detonation engines - Thrust augmentation
Edition Identifiers:
- The Open Library ID: OL16094153M
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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8Preliminary dynamic tests of a flight-type ejector
By Colin K. Drummond
“Preliminary dynamic tests of a flight-type ejector” Metadata:
- Title: ➤ Preliminary dynamic tests of a flight-type ejector
- Author: Colin K. Drummond
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - For sale by the National Technical Information Service
- Publish Date: 1992
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Preliminary dynamic tests of a flight-type ejector” Subjects and Themes:
- Subjects: ➤ Ejectors - Short take-off and landing aircraft - Jet propulsion
Edition Identifiers:
- The Open Library ID: OL15366246M
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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9Transient flow thrust prediction for an ejector propulsion concept
By Colin K. Drummond
“Transient flow thrust prediction for an ejector propulsion concept” Metadata:
- Title: ➤ Transient flow thrust prediction for an ejector propulsion concept
- Author: Colin K. Drummond
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - For sale by the National Technical Information Service
- Publish Date: 1989
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Transient flow thrust prediction for an ejector propulsion concept” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL15294123M
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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10Parametric 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
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11A 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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12Combined numerical/analytical perturbation solutions of the Navier-Stokes equations for aerodynamic ejector/mixer nozzle flows
By Lawrence Justin DeChant
“Combined numerical/analytical perturbation solutions of the Navier-Stokes equations for aerodynamic ejector/mixer nozzle flows” Metadata:
- Title: ➤ Combined numerical/analytical perturbation solutions of the Navier-Stokes equations for aerodynamic ejector/mixer nozzle flows
- Author: Lawrence Justin DeChant
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Combined numerical/analytical perturbation solutions of the Navier-Stokes equations for aerodynamic ejector/mixer nozzle flows” Subjects and Themes:
- Subjects: ➤ Ejectors - Mixing layers (Fluids) - Jet propulsion - Navier-Stokes equation - Mixers - Fluid mechanics - Computer programs - Nozzle design - Supersonic transports
Edition Identifiers:
- The Open Library ID: OL15507691M
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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13Lobed mixer optimization for advanced ejector geometries
By Ian A. Waitz
“Lobed mixer optimization for advanced ejector geometries” Metadata:
- Title: ➤ Lobed mixer optimization for advanced ejector geometries
- Author: Ian A. Waitz
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Lobed mixer optimization for advanced ejector geometries” Subjects and Themes:
- Subjects: ➤ Mixing - Numerical analysis - Geometry - Ejectors - Data acquisition - Experimentation
Edition Identifiers:
- The Open Library ID: OL15491194M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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14Acoustic and aerothermal performance test of the axisymmetric coannular ejector nozzle
By William Herkes
“Acoustic and aerothermal performance test of the axisymmetric coannular ejector nozzle” Metadata:
- Title: ➤ Acoustic and aerothermal performance test of the axisymmetric coannular ejector nozzle
- Author: William Herkes
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - National Technical Information Service [distributor - Available from NASA Center for AeroSpace Information
- Publish Date: 2000
- Publish Location: ➤ [Cleveland, Ohio] - Springfield, VA - Hanover, MD
“Acoustic and aerothermal performance test of the axisymmetric coannular ejector nozzle” Subjects and Themes:
- Subjects: ➤ Noise - Aeroacoustics - Plug nozzles - Jet nozzles - Wind tunnel tests - Performance tests - Acoustic properties - Aerodynamic noise - Noise reduction - Effective perceived noise levels - Jet planes - Ejectors - Jet aircraft noise
Edition Identifiers:
- The Open Library ID: OL15572747M
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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15Unsteady ejector performance
By Daniel E. Paxson
“Unsteady ejector performance” Metadata:
- Title: Unsteady ejector performance
- Author: Daniel E. Paxson
- Language: English
- Publisher: ➤ Available from NASA Center for AeroSpace Information - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2002
- Publish Location: Cleveland, Ohio - Hanover MD
“Unsteady ejector performance” Subjects and Themes:
- Subjects: ➤ Intake systems - Unsteady flow - Pulsejet engines - Thrust augmentation - Ejectors - Propulsion system performance
Edition Identifiers:
- The Open Library ID: OL16053813M
Access and General Info:
- First Year Published: 2002
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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16Effect of delta tabs on free jets from complex nozzles
By K. B. M. Q. Zaman
“Effect of delta tabs on free jets from complex nozzles” Metadata:
- Title: ➤ Effect of delta tabs on free jets from complex nozzles
- Author: K. B. M. Q. Zaman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - Available from NASA Center for Aerospace Information
- Publish Date: 2001
- Publish Location: ➤ [Cleveland, Ohio] - Hanover, MD
“Effect of delta tabs on free jets from complex nozzles” Subjects and Themes:
- Subjects: ➤ Ejectors - Flow distribution - Nozzle flow - Tabs (Control surfaces) - Free jets - Simulation
Edition Identifiers:
- The Open Library ID: OL16048239M
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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17Phase 4 static tests of the J-97 powered, external augmentor V/STOL model at the NASA, Ames Research Center, November 1983
By D. B. Garland
“Phase 4 static tests of the J-97 powered, external augmentor V/STOL model at the NASA, Ames Research Center, November 1983” Metadata:
- Title: ➤ Phase 4 static tests of the J-97 powered, external augmentor V/STOL model at the NASA, Ames Research Center, November 1983
- Author: D. B. Garland
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1988
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va
“Phase 4 static tests of the J-97 powered, external augmentor V/STOL model at the NASA, Ames Research Center, November 1983” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Ejectors - Short take-off and landing aircraft - Jet propulsion
Edition Identifiers:
- The Open Library ID: OL17659876M
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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18Simulated flight acoustic investigtion of treated ejector effectiveness on advanced mechanical suppressors for high velocity jet noise reduction
By John F. Brausch
“Simulated flight acoustic investigtion of treated ejector effectiveness on advanced mechanical suppressors for high velocity jet noise reduction” Metadata:
- Title: ➤ Simulated flight acoustic investigtion of treated ejector effectiveness on advanced mechanical suppressors for high velocity jet noise reduction
- Author: John F. Brausch
- Number of Pages: Median: 408
- Publisher: Lewis Research Center
- Publish Date: 1986
- Publish Location: Cleveland, Ohio
“Simulated flight acoustic investigtion of treated ejector effectiveness on advanced mechanical suppressors for high velocity jet noise reduction” Subjects and Themes:
- Subjects: Nozzles - Ejectors - Jet aircraft noise - Variable cycle engines
Edition Identifiers:
- The Open Library ID: OL20985942M
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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19Design and calibration of an air ejector to operate against various back pressures
By Ronald G. A. Chisholm
“Design and calibration of an air ejector to operate against various back pressures” Metadata:
- Title: ➤ Design and calibration of an air ejector to operate against various back pressures
- Author: Ronald G. A. Chisholm
- Number of Pages: Median: 38
- Publisher: Institute of Aerophysics
- Publish Date: 1960
- Publish Location: [Downsview, Ont.]
“Design and calibration of an air ejector to operate against various back pressures” Subjects and Themes:
- Subjects: Jet pumps - Ejectors - GETOL aircraft
Edition Identifiers:
- The Open Library ID: OL19004043M
Access and General Info:
- First Year Published: 1960
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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