Explore: Engine Inlets
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Source: The Open Library
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1Improved NASA-ANOPP noise prediction computer code for advanced subsonic propulsion systems
By K. B. Kontos
“Improved NASA-ANOPP noise prediction computer code for advanced subsonic propulsion systems” Metadata:
- Title: ➤ Improved NASA-ANOPP noise prediction computer code for advanced subsonic propulsion systems
- Author: K. B. Kontos
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Technical Information Service [distributor - National Aeronautics and Space Administration
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Improved NASA-ANOPP noise prediction computer code for advanced subsonic propulsion systems” Subjects and Themes:
- Subjects: ➤ Engine inlets - Pressure reduction - Aircraft noise - Aerodynamic noise - Noise reduction - Noise prediction - Engine noise
Edition Identifiers:
- The Open Library ID: OL18111692M - OL17122758M - OL15479071M - OL17546956M
- Online Computer Library Center (OCLC) ID: 38860517
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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2Finite element elastic-plastic-creep and cyclic life analysis of a cowl lip
By V. K. Arya
“Finite element elastic-plastic-creep and cyclic life analysis of a cowl lip” Metadata:
- Title: ➤ Finite element elastic-plastic-creep and cyclic life analysis of a cowl lip
- Author: V. K. Arya
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration
- Publish Date: 1990
- Publish Location: [Washington, D.C.]
“Finite element elastic-plastic-creep and cyclic life analysis of a cowl lip” Subjects and Themes:
- Subjects: ➤ Finite element method - Strain distribution - Stress distribution - Engine inlets - Life (Durability) - Leading edges - Stress concentration
Edition Identifiers:
- The Open Library ID: OL20571067M - OL17630361M - OL18250118M - OL17725732M
- Online Computer Library Center (OCLC) ID: 62869280
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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3Development of a low-Reynolds number, nonlinear [kappa-epsilon] model for the reduced Navier-Stokes equations
By David A. Boger
“Development of a low-Reynolds number, nonlinear [kappa-epsilon] model for the reduced Navier-Stokes equations” Metadata:
- Title: ➤ Development of a low-Reynolds number, nonlinear [kappa-epsilon] model for the reduced Navier-Stokes equations
- Author: David A. Boger
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Development of a low-Reynolds number, nonlinear [kappa-epsilon] model for the reduced Navier-Stokes equations” Subjects and Themes:
- Subjects: ➤ Viscous flow - Turbulent flow - Boundary layer separation - Low Reynolds number - Vortex generators - Predictions - Navier-Stokes equation - Engine inlets - Aircraft engines - K-epsilon turbulence model
Edition Identifiers:
- The Open Library ID: OL17122720M - OL18116007M - OL15491180M - OL17540932M
- Online Computer Library Center (OCLC) ID: 38840668
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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4IPAC--Inlet Performance Analysis Code
By Paul J. Barnhart
“IPAC--Inlet Performance Analysis Code” Metadata:
- Title: ➤ IPAC--Inlet Performance Analysis Code
- Author: Paul J. Barnhart
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“IPAC--Inlet Performance Analysis Code” Subjects and Themes:
- Subjects: ➤ Engine inlets - Inlet flow - Aerodynamic coefficients - Pressure recovery - Aerodynamic drag - Reliability analysis
Edition Identifiers:
- The Open Library ID: OL18115388M - OL17564997M - OL17123843M - OL15489478M
- Online Computer Library Center (OCLC) ID: 39289699
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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5Performance study for inlet installations
By D. C. Bingaman
“Performance study for inlet installations” Metadata:
- Title: ➤ Performance study for inlet installations
- Author: D. C. Bingaman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1992
- Publish Location: [Springfield, Va - Hampton, Va
“Performance study for inlet installations” Subjects and Themes:
- Subjects: ➤ Aircraft performance - Engine airframe integration - Aircraft design - Wind tunnel tests - Bomber aircraft - Design analysis - Engine inlets - Aircraft detection - McDonnell aircraft - Fighter aircraft - Inlet airframe configurations
Edition Identifiers:
- The Open Library ID: OL15413640M - OL17791633M
- Online Computer Library Center (OCLC) ID: 33389420
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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6Rocket-based combined cycle engine technology development
By J. R. DeBonis
“Rocket-based combined cycle engine technology development” Metadata:
- Title: ➤ Rocket-based combined cycle engine technology development
- Author: J. R. DeBonis
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center, Ohio Aerospace Institute, Institute for Computational Mechanics in Propulsion - National Aeronautics and Space Administration, distributor]
- Publish Date: 1996
- Publish Location: ➤ [Cleveland, Ohio] - [Springfield, Va
“Rocket-based combined cycle engine technology development” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Computational grids - Engine inlets - Flow distribution - Hypersonic flow - Navier-Stokes equation - Pressure distribution - Rocket engine design - Rocket engines - Static pressure
Edition Identifiers:
- The Open Library ID: OL17593984M - OL18121288M - OL15504564M
- Online Computer Library Center (OCLC) ID: 41375980
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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7NASA Lewis Propulsion Systems Laboratory customer guide manual
By Ronald H. Soeder
“NASA Lewis Propulsion Systems Laboratory customer guide manual” Metadata:
- Title: ➤ NASA Lewis Propulsion Systems Laboratory customer guide manual
- Author: Ronald H. Soeder
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“NASA Lewis Propulsion Systems Laboratory customer guide manual” Subjects and Themes:
- Subjects: ➤ Propulsion system configurations - Engine tests - Propulsion system performance - NASA programs - Flight simulation - Turbine engines - Test equipment - Support systems - Engineering management - Laboratory equipment - Gas turbine engines - Operations research - Test facilities - Engine inlets - Engine design - Manuals - Full scale tests - Performance tests - Aircraft engines - Altitude
Edition Identifiers:
- The Open Library ID: OL15404441M - OL17682993M - OL17790359M
- Online Computer Library Center (OCLC) ID: 32309302
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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8Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow
By Kenneth J. Baumeister
“Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow” Metadata:
- Title: ➤ Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow
- Author: Kenneth J. Baumeister
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Aircraft engines - Ducted flow - Engine inlets - Finite difference theory - Iterative solution - Real time operation - Sound propagation
Edition Identifiers:
- The Open Library ID: OL17565459M - OL15497519M - OL18118423M
- Online Computer Library Center (OCLC) ID: 39725963
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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9An investigation of bleed configurations and their effect on shock wave/boundary layer interactions
By A. Hamed
“An investigation of bleed configurations and their effect on shock wave/boundary layer interactions” Metadata:
- Title: ➤ An investigation of bleed configurations and their effect on shock wave/boundary layer interactions
- 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
“An investigation of bleed configurations and their effect on shock wave/boundary layer interactions” Subjects and Themes:
- Subjects: ➤ Corner flow - Engine design - Engine inlets - Oblique shock waves - Secondary flow - Separated flow - Shock wave interaction - Supersonic inlets
Edition Identifiers:
- The Open Library ID: OL15418954M - OL17793974M
- Online Computer Library Center (OCLC) ID: 34562841
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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10Comparison of the aeroacoustics of two small-scale supersonic inlets
By Wing Ng
“Comparison of the aeroacoustics of two small-scale supersonic inlets” Metadata:
- Title: ➤ Comparison of the aeroacoustics of two small-scale supersonic inlets
- Author: Wing Ng
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Comparison of the aeroacoustics of two small-scale supersonic inlets” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Aircraft engines - Engine inlets - Flow distribution - Flow measurement - Inlet flow - Mach number - Supersonic inlets
Edition Identifiers:
- The Open Library ID: OL17593732M - OL15508989M
- Online Computer Library Center (OCLC) ID: 41272155
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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11Control of flow separation and mixing by aerodynamic excitation
By Edward J. Rice
“Control of flow separation and mixing by aerodynamic excitation” Metadata:
- Title: ➤ Control of flow separation and mixing by aerodynamic excitation
- Author: Edward J. Rice
- 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
“Control of flow separation and mixing by aerodynamic excitation” Subjects and Themes:
- Subjects: ➤ Shear flow - Inlet flow - Shear layers - Separated flow - Boundary layer separation - Coanda effect - Engine inlets - Aircraft engines - Airfoils - Mixing - Turbulence effects - Unsteady aerodynamics
Edition Identifiers:
- The Open Library ID: OL16135113M - OL17634399M
- Online Computer Library Center (OCLC) ID: 24985892
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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12Mach 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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133D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
By M. Mizukami
“3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Metadata:
- Title: ➤ 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
- Author: M. Mizukami
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Boundary layers - Supersonic diffusers - Computational grids - Boundary layer separation - Turbulence models - Three dimensional flow - Flow distribution - Engine inlets - Internal flow - Leading edges - Shock wave interaction - Navier-Stokes equation - Shock waves
Edition Identifiers:
- The Open Library ID: OL17117540M - OL17106503M
- Online Computer Library Center (OCLC) ID: 35282961
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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14Collection efficiency and ice accretion calculations for a Boeing 737-300 inlet
By Colin S. Bidwell
“Collection efficiency and ice accretion calculations for a Boeing 737-300 inlet” Metadata:
- Title: ➤ Collection efficiency and ice accretion calculations for a Boeing 737-300 inlet
- Author: Colin S. Bidwell
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Collection efficiency and ice accretion calculations for a Boeing 737-300 inlet” Subjects and Themes:
- Subjects: Boeing 737 aircraft - Ice formation - Engine inlets - Prediction analysis techniques - Inlet pressure
Edition Identifiers:
- The Open Library ID: OL15452220M - OL17806198M
- Online Computer Library Center (OCLC) ID: 37496012
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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15Collection efficiency and ice accretion calculations for a sphere, a swept MS(1)-317 wing, a swept NACA-0012 wing tip, an axisymmetric inlet, and a Boeing 737-300 inlet
By Colin S. Bidwell
“Collection efficiency and ice accretion calculations for a sphere, a swept MS(1)-317 wing, a swept NACA-0012 wing tip, an axisymmetric inlet, and a Boeing 737-300 inlet” Metadata:
- Title: ➤ Collection efficiency and ice accretion calculations for a sphere, a swept MS(1)-317 wing, a swept NACA-0012 wing tip, an axisymmetric inlet, and a Boeing 737-300 inlet
- Author: Colin S. Bidwell
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Collection efficiency and ice accretion calculations for a sphere, a swept MS(1)-317 wing, a swept NACA-0012 wing tip, an axisymmetric inlet, and a Boeing 737-300 inlet” Subjects and Themes:
- Subjects: Aircraft icing - Engine inlets - Swept wings - Accumulations - Spheres
Edition Identifiers:
- The Open Library ID: OL15411096M - OL17790929M
- Online Computer Library Center (OCLC) ID: 32869193
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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16Wind-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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173D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
By Masashi Mizukami
“3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Metadata:
- Title: ➤ 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
- Author: Masashi Mizukami
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Boundary layers - Supersonic diffusers - Computational grids - Boundary layer separation - Turbulence models - Three dimensional flow - Flow distribution - Engine inlets - Internal flow - Leading edges - Shock wave interaction - Navier-Stokes equation - Shock waves
Edition Identifiers:
- The Open Library ID: OL18086923M - OL15423278M
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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18Finite difference time marching in the frequency domain
By Kenneth J. Baumeister
“Finite difference time marching in the frequency domain” Metadata:
- Title: ➤ Finite difference time marching in the frequency domain
- Author: Kenneth J. Baumeister
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, D.C - Springfield, Va - [Washington, DC
“Finite difference time marching in the frequency domain” Subjects and Themes:
- Subjects: ➤ Acoustics - Aircraft engines - Ducts - Engine inlets - Finite difference theory - Nacelles - Partial Differential equations - Sound propagation - Time dependence - Time marching - Wave equations
Edition Identifiers:
- The Open Library ID: OL15505882M - OL15503807M
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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19Multigrid methods for aerodynamic problems in complex geometries
By D. A. Caughey
“Multigrid methods for aerodynamic problems in complex geometries” Metadata:
- Title: ➤ Multigrid methods for aerodynamic problems in complex geometries
- Author: D. A. Caughey
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“Multigrid methods for aerodynamic problems in complex geometries” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Engine inlets - Euler equations of motion - Finite volume method - Inviscid flow - Multiblock grids - Multigrid methods - Navier-Stokes equation - Three dimensional flow - Transonic flow - Viscous flow
Edition Identifiers:
- The Open Library ID: OL15419815M
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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20High Reynolds number investigation of a flush-mounted, S-duct inlet with large amounts of boundary layer ingestion
By Bobby L. Berrier
“High Reynolds number investigation of a flush-mounted, S-duct inlet with large amounts of boundary layer ingestion” Metadata:
- Title: ➤ High Reynolds number investigation of a flush-mounted, S-duct inlet with large amounts of boundary layer ingestion
- Author: Bobby L. Berrier
- Language: English
- Number of Pages: Median: 165
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 2005
- Publish Location: Hampton, Va
“High Reynolds number investigation of a flush-mounted, S-duct inlet with large amounts of boundary layer ingestion” Subjects and Themes:
- Subjects: Boundary layers - Aerodynamic configurations - Air flow - Ducts - Engine inlets
Edition Identifiers:
- The Open Library ID: OL43928567M
- Online Computer Library Center (OCLC) ID: 793417465
Access and General Info:
- First Year Published: 2005
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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21Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach
By W. P. Norby
“Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach” Metadata:
- Title: ➤ Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach
- Author: W. P. Norby
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Inlet flow - Computational grids - Pressure distribution - Turbulence models - Flow distortion - Flow distribution - Engine inlets - Aircraft engines - Angle of attack - Turbulence effects
Edition Identifiers:
- The Open Library ID: OL15490315M
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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22Application of CFD to the analysis and design of high-speed inlets
By William C. Rose
“Application of CFD to the analysis and design of high-speed inlets” Metadata:
- Title: ➤ Application of CFD to the analysis and design of high-speed inlets
- Author: William C. Rose
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Application of CFD to the analysis and design of high-speed inlets” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Engine design - Histories - Engine inlets - Hypersonic speed - Computer aided design - Computer programs - High speed
Edition Identifiers:
- The Open Library ID: OL15413873M
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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23SSME fuelside preburner two-dimensional analysis
By Thomas J. Van Overbeke
“SSME fuelside preburner two-dimensional analysis” Metadata:
- Title: ➤ SSME fuelside preburner two-dimensional analysis
- Author: Thomas J. Van Overbeke
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1986
- Publish Location: [Cleveland, Ohio
“SSME fuelside preburner two-dimensional analysis” Subjects and Themes:
- Subjects: ➤ Computer programs - Engine inlets - Flow distribution - Preburners - Propulsion systems - Space shuttle main engine - Space shuttles
Edition Identifiers:
- The Open Library ID: OL17727115M
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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24Wind-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
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25Three dimensional compressible turbulent flow computations for a diffusing S-duct with/without vortex generators
By Soo-Yong Cho
“Three dimensional compressible turbulent flow computations for a diffusing S-duct with/without vortex generators” Metadata:
- Title: ➤ Three dimensional compressible turbulent flow computations for a diffusing S-duct with/without vortex generators
- Author: Soo-Yong Cho
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1994
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Three dimensional compressible turbulent flow computations for a diffusing S-duct with/without vortex generators” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Turbulent flow - Inlet flow - Subsonic flow - Viscous flow - Vortices - Duct geometry - Three dimensional flow - Finite volume method - Navier-Stokes equation - Engine inlets - Compressible flow - Vortex generators
Edition Identifiers:
- The Open Library ID: OL15408550M
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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26Fan noise prediction assessment
By Paul H. Bent
“Fan noise prediction assessment” Metadata:
- Title: ➤ Fan noise prediction assessment
- Author: Paul H. Bent
- 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
“Fan noise prediction assessment” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Directivity - Engine inlets - Noise prediction (Aircraft) - Finite element method - Aerodynamic noise - Engine noise - Nacelles
Edition Identifiers:
- The Open Library ID: OL15423091M
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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27Final technical report on grant NAG3-1567 entitled Inlet distortion in engines on VSTOL aircraft
By Choon Sooi Tan
“Final technical report on grant NAG3-1567 entitled Inlet distortion in engines on VSTOL aircraft” Metadata:
- Title: ➤ Final technical report on grant NAG3-1567 entitled Inlet distortion in engines on VSTOL aircraft
- Author: Choon Sooi Tan
- Language: English
- Publisher: ➤ The Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ Cleveland, OH - [Springfield, Va
“Final technical report on grant NAG3-1567 entitled Inlet distortion in engines on VSTOL aircraft” Subjects and Themes:
- Subjects: ➤ Engine inlets - Flow distortion - Nonuniform flow - V/STOL aircraft - Three dimensional flow - Inlet flow - Turbocompressors
Edition Identifiers:
- The Open Library ID: OL18075768M
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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28Fan noise prediction system development
By H. D. Meyer
“Fan noise prediction system development” Metadata:
- Title: ➤ Fan noise prediction system development
- Author: H. D. Meyer
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1993
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Fan noise prediction system development” Subjects and Themes:
- Subjects: ➤ Fan blades - Acoustic propagation - Far fields - Computerized simulation - Digital simulation - Applications programs (Computers) - Engine inlets - Aerodynamic noise - Turbofan engines - Finite element method
Edition Identifiers:
- The Open Library ID: OL15505669M
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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29Improved finite element modeling of the turbofan engine inlet radiation problem
By Indranil Danda Roy
“Improved finite element modeling of the turbofan engine inlet radiation problem” Metadata:
- Title: ➤ Improved finite element modeling of the turbofan engine inlet radiation problem
- Author: Indranil Danda Roy
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1993
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Improved finite element modeling of the turbofan engine inlet radiation problem” Subjects and Themes:
- Subjects: ➤ Far fields - Computerized simulation - Digital simulation - Mathematical models - Engine inlets - Finite element method - Turbofan engines - Numerical flow visualization - Sound waves
Edition Identifiers:
- The Open Library ID: OL15505672M
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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30Effects of initial conditions on a single jet in crossflow
By D. S. Liscinsky
“Effects of initial conditions on a single jet in crossflow” Metadata:
- Title: ➤ Effects of initial conditions on a single jet in crossflow
- Author: D. S. Liscinsky
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Effects of initial conditions on a single jet in crossflow” Subjects and Themes:
- Subjects: ➤ Engine inlets - Mixing - Inlet flow - Swirling - Jet flow - Jet mixing flow - Cross flow
Edition Identifiers:
- The Open Library ID: OL15414473M
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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31Numerical analysis of the trailblazer inlet flowfield for hypersonic Mach numbers
By C. J. Steffen
“Numerical analysis of the trailblazer inlet flowfield for hypersonic Mach numbers” Metadata:
- Title: ➤ Numerical analysis of the trailblazer inlet flowfield for hypersonic Mach numbers
- Author: C. J. Steffen
- 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
“Numerical analysis of the trailblazer inlet flowfield for hypersonic Mach numbers” Subjects and Themes:
- Subjects: Engine inlets - Numerical analysis - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15571746M
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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32Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attack
By Crawford F. Smith
“Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attack” Metadata:
- Title: ➤ Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attack
- Author: Crawford F. Smith
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attack” Subjects and Themes:
- Subjects: ➤ Intake systems - Inlet flow - F-18 aircraft - Wind tunnel tests - Wind tunnels - Flow distribution - Engine inlets - Air flow - Wind tunnel walls - Angle of attack
Edition Identifiers:
- The Open Library ID: OL15409179M
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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33PARC3D calculations of the F/A-18A HARV inlet vortex generators
By Steve D. Podleski
“PARC3D calculations of the F/A-18A HARV inlet vortex generators” Metadata:
- Title: ➤ PARC3D calculations of the F/A-18A HARV inlet vortex generators
- Author: Steve D. Podleski
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“PARC3D calculations of the F/A-18A HARV inlet vortex generators” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Flow distortion - F-18 aircraft - Separated flow - Computational grids - Vortex generators - Applications programs (Computers) - Transonic speed - Engine inlets - Maneuverability - Research vehicles
Edition Identifiers:
- The Open Library ID: OL15425817M
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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34Computational analysis in support of the SSTO flowpath test
By Beverly S. Duncan
“Computational analysis in support of the SSTO flowpath test” Metadata:
- Title: ➤ Computational analysis in support of the SSTO flowpath test
- Author: Beverly S. Duncan
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1994
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Computational analysis in support of the SSTO flowpath test” Subjects and Themes:
- Subjects: ➤ Engine inlets - Inlet flow - Diverters - Hypersonic inlets - Boundary layer flow - Cowlings
Edition Identifiers:
- The Open Library ID: OL17114580M
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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35A design strategy for the use of vortex generators to manage inlet-engine distortion using computational fluid dynamics
By Bernhard H. Anderson
“A design strategy for the use of vortex generators to manage inlet-engine distortion using computational fluid dynamics” Metadata:
- Title: ➤ A design strategy for the use of vortex generators to manage inlet-engine distortion using computational fluid dynamics
- Author: Bernhard H. Anderson
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1991
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“A design strategy for the use of vortex generators to manage inlet-engine distortion using computational fluid dynamics” Subjects and Themes:
- Subjects: Engine inlets - Flow distortion - Vortex generators - Flow distribution - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL15399186M
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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36A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92
By Richard J. Re
“A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92” Metadata:
- Title: ➤ A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92
- Author: Richard J. Re
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1996
- Publish Location: Hampton, Va - [Springfield, Va
“A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92” Subjects and Themes:
- Subjects: ➤ Static pressure - Pressure distribution - Wind tunnel tests - Subsonic flow - Angle of attack - Engine inlets - Aircraft engines - Mach number
Edition Identifiers:
- The Open Library ID: OL15498125M
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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37Method for extracting forward acoustic wave components from rotating microphone measurements in the inlets of turbofan engines
By D. E. Cicon
“Method for extracting forward acoustic wave components from rotating microphone measurements in the inlets of turbofan engines” Metadata:
- Title: ➤ Method for extracting forward acoustic wave components from rotating microphone measurements in the inlets of turbofan engines
- Author: D. E. Cicon
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Method for extracting forward acoustic wave components from rotating microphone measurements in the inlets of turbofan engines” Subjects and Themes:
- Subjects: ➤ Microphones - Sound fields - Aeroacoustics - Engine inlets - Acoustic measurement - Sound propagation - Turbofan engines - Engine monitoring instruments
Edition Identifiers:
- The Open Library ID: OL15414596M
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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38A numerical analysis applied to high angle of attack three-dimensional inlets
By Danny P. Hwang
“A numerical analysis applied to high angle of attack three-dimensional inlets” Metadata:
- Title: ➤ A numerical analysis applied to high angle of attack three-dimensional inlets
- Author: Danny P. Hwang
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1986
- Publish Location: [Cleveland, Ohio
“A numerical analysis applied to high angle of attack three-dimensional inlets” Subjects and Themes:
- Subjects: ➤ Angle of attack - Angle of attack (Aerodynamics) - Computational fluid dynamics - Engine inlets - Fluid dynamics - Inlet flow - Panel method (Fluid dynamics) - Potential flow - Separated flow
Edition Identifiers:
- The Open Library ID: OL16151159M
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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