Explore: Inlet Flow
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Source: The Open Library
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1Numerical simulation of the flow about the F-18 HARV at high angle of attack
By Scott M. Murman
“Numerical simulation of the flow about the F-18 HARV at high angle of attack” Metadata:
- Title: ➤ Numerical simulation of the flow about the F-18 HARV at high angle of attack
- Author: Scott M. Murman
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - MCAT Institute - National Aeronautics and Space Administration
- Publish Date: 1994 - 1995
- Publish Location: ➤ [Washington, D.C - Springfield, Va - [Washington, DC - San Jose, CA
“Numerical simulation of the flow about the F-18 HARV at high angle of attack” Subjects and Themes:
- Subjects: ➤ Angle of attack - Computational fluid dynamics - Computational grids - Computerized simulation - F-18 aircraft - Flow geometry - Grid generation (Mathematics) - High Reynolds number - Inlet flow - Leading edge flaps - Mathematical models - Navier-Stokes equation - Numerical analysis - Research aircraft - Research vehicles - Vortex shedding - Vortices
Edition Identifiers:
- The Open Library ID: ➤ OL17683979M - OL17788522M - OL18062579M - OL18081181M - OL17679545M - OL17791646M - OL17683434M - OL17792265M
- Online Computer Library Center (OCLC) ID: 32650521 - 33870418 - 34765697
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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2A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application
By Kamlesh Kapoor
“A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application” Metadata:
- Title: ➤ A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application
- Author: Kamlesh Kapoor
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Bypasses - Flow distortion - Civil aviation - Cross flow - Inlet flow - Diffusers - Navier-Stokes equation - Mass flow - Supersonic inlets - Supersonic diffusers - Supersonic transports
Edition Identifiers:
- The Open Library ID: OL17114056M - OL17002076M - OL18076587M - OL15404445M
- Online Computer Library Center (OCLC) ID: 32309713
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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3Reduction of Blade-Vortex Interaction (BVI) noise through X-force control
By Fredric H. Schmitz
“Reduction of Blade-Vortex Interaction (BVI) noise through X-force control” Metadata:
- Title: ➤ Reduction of Blade-Vortex Interaction (BVI) noise through X-force control
- Author: Fredric H. Schmitz
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1995
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va
“Reduction of Blade-Vortex Interaction (BVI) noise through X-force control” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Aircraft landing - Blade slap noise - Blade-vortex interaction - Flight control - Flight paths - Helicopters - Inlet flow - Longitudinal stability - Noise prediction (Aircraft) - Noise reduction
Edition Identifiers:
- The Open Library ID: OL18087419M - OL15424058M - OL17106597M - OL17117531M
- Online Computer Library Center (OCLC) ID: 35280105
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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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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5Installed F/A-18 inlet flow calculations at 30 degrees angle-of-attack, a comparative study
By C. Frederic Smith
“Installed F/A-18 inlet flow calculations at 30 degrees angle-of-attack, a comparative study” Metadata:
- Title: ➤ Installed F/A-18 inlet flow calculations at 30 degrees angle-of-attack, a comparative study
- Author: C. Frederic Smith
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Lewis Research Center
- Publish Date: 1994
- Publish Location: ➤ [Cleveland, Ohio] - Springfield, Va - [Washington, DC
“Installed F/A-18 inlet flow calculations at 30 degrees angle-of-attack, a comparative study” Subjects and Themes:
- Subjects: ➤ Angle of attack - F-18 aircraft - Highly maneuverable aircraft - Inlet airframe configurations - Inlet flow - Research vehicles - Subsonic speed - Vortices
Edition Identifiers:
- The Open Library ID: OL17000516M - OL18075553M - OL15401957M
- Online Computer Library Center (OCLC) ID: 32062761
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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6Research on a two-dimensional inlet for a supersonic V/STOL propulsion system
By J. L. Mark
“Research on a two-dimensional inlet for a supersonic V/STOL propulsion system” Metadata:
- Title: ➤ Research on a two-dimensional inlet for a supersonic V/STOL propulsion system
- Author: J. L. Mark
- Language: English
- Publisher: ➤ McDonnell Aircraft Company, McDonnell Douglas Corporation - National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1989
- Publish Location: ➤ [Cleveland, Ohio] - St. Louis, Mo.]
“Research on a two-dimensional inlet for a supersonic V/STOL propulsion system” Subjects and Themes:
- Subjects: Performance tests - Inlet flow - Aircraft design - V/STOL aircraft - Design analysis
Edition Identifiers:
- The Open Library ID: OL18263876M - OL17634650M - OL16138646M
- Online Computer Library Center (OCLC) ID: 70141386
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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7Comparison 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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8Theoretical and experimental study of flow-control devices for inlets of indraft wind tunnels
By James C. Ross
“Theoretical and experimental study of flow-control devices for inlets of indraft wind tunnels” Metadata:
- Title: ➤ Theoretical and experimental study of flow-control devices for inlets of indraft wind tunnels
- Author: James C. Ross
- Language: English
- Number of Pages: Median: 66
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1989
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va
“Theoretical and experimental study of flow-control devices for inlets of indraft wind tunnels” Subjects and Themes:
- Subjects: ➤ Wind tunnels - Design and construction - Guide vanes - Velocity distribution - Inlet flow - Flow distortion - Flow distribution
Edition Identifiers:
- The Open Library ID: OL17633851M - OL17726036M
- Online Computer Library Center (OCLC) ID: 25206537
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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9LDV measurements in an annular combustor model
By Dean A. Barron
“LDV measurements in an annular combustor model” Metadata:
- Title: ➤ LDV measurements in an annular combustor model
- Author: Dean A. Barron
- Language: English
- Publisher: ➤ Purdue University, School of Aeronautics and Astronautics - For sale by the National Technical Information Service - National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1989 - 1996
- Publish Location: ➤ [Washington, DC] - West Lafayette, Ind - [Springfield, Va
“LDV measurements in an annular combustor model” Subjects and Themes:
- Subjects: ➤ Annular flow - Combustion chambers - Inlet flow - Laser Doppler velocimeters - Lasers - Turbulence - Turbulent flow - Velocity measurement - Viscous damping - Viscous flow
Edition Identifiers:
- The Open Library ID: OL15289378M - OL15492271M
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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10Control 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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11Mach 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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12Numerical simulation of supersonic and hypersonic inlet flow fields
By D. Scott McRae
“Numerical simulation of supersonic and hypersonic inlet flow fields” Metadata:
- Title: ➤ Numerical simulation of supersonic and hypersonic inlet flow fields
- Author: D. Scott McRae
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Mars Mission Research Center, North Carolina State University
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC - Raleigh, N.C - Springfield, Va
“Numerical simulation of supersonic and hypersonic inlet flow fields” Subjects and Themes:
- Subjects: ➤ Algorithms - Computational fluid dynamics - Computational grids - Flow distribution - Grid generation (Mathematics) - Hypersonic inlets - Inlet flow - Inviscid flow - Supersonic inlets - Three dimensional flow - Upwind schemes (Mathematics)
Edition Identifiers:
- The Open Library ID: OL15418943M - OL17793972M
- Online Computer Library Center (OCLC) ID: 34562883
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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13Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code
By Kamlesh Kapoor
“Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code” Metadata:
- Title: ➤ Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code
- Author: Kamlesh Kapoor
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Inlet flow - Two dimensional flow - Corner flow - Hypersonic inlets - Turbulent boundary layer - Hypersonic speed - Supersonic speed - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15409264M - OL17788471M
- Online Computer Library Center (OCLC) ID: 32731299
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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14An experimental device for generating high frequency perturbations in supersonic wind tunnels
By Kevin J. Melcher
“An experimental device for generating high frequency perturbations in supersonic wind tunnels” Metadata:
- Title: ➤ An experimental device for generating high frequency perturbations in supersonic wind tunnels
- Author: Kevin J. Melcher
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“An experimental device for generating high frequency perturbations in supersonic wind tunnels” Subjects and Themes:
- Subjects: ➤ Gusts - Inlet flow - Supersonic wind tunnels - Pressure pulses - Surges - Wind tunnel apparatus
Edition Identifiers:
- The Open Library ID: OL15497563M - OL17834504M
- Online Computer Library Center (OCLC) ID: 39728855
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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15Wind-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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16Inlet flow characteristics during rapid maneuvers for an F/A-18A airplane
By William G. Steenken
“Inlet flow characteristics during rapid maneuvers for an F/A-18A airplane” Metadata:
- Title: ➤ Inlet flow characteristics during rapid maneuvers for an F/A-18A airplane
- Author: William G. Steenken
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: ➤ Edwards, Calif - [Springfield, Va
“Inlet flow characteristics during rapid maneuvers for an F/A-18A airplane” Subjects and Themes:
- Subjects: ➤ Air flow - Air intakes - Flow characteristics - Inlet flow - Intake systems - Research aircraft
Edition Identifiers:
- The Open Library ID: OL17592566M - OL15560462M
- Online Computer Library Center (OCLC) ID: 43452237
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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17Estimating engine airflow in gas-turbine powered aircraft with clean and distorted inlet flows
By Williams, J. G.
“Estimating engine airflow in gas-turbine powered aircraft with clean and distorted inlet flows” Metadata:
- Title: ➤ Estimating engine airflow in gas-turbine powered aircraft with clean and distorted inlet flows
- Author: Williams, J. G.
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ Edwards, Calif - [Springfield, Va
“Estimating engine airflow in gas-turbine powered aircraft with clean and distorted inlet flows” Subjects and Themes:
- Subjects: ➤ Air flow - Engine tests - F-18 aircraft - Flow distortion - Flow measurement - Flow velocity - Gas turbine engines - Inlet flow - Inlet pressure - Static pressure - Turbofans
Edition Identifiers:
- The Open Library ID: OL15504888M
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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18Starvation effects on the hydrodynamic lubrication of rigid nonconformal contacts in combined rolling and normal motion
By M. K. Ghosh
“Starvation effects on the hydrodynamic lubrication of rigid nonconformal contacts in combined rolling and normal motion” Metadata:
- Title: ➤ Starvation effects on the hydrodynamic lubrication of rigid nonconformal contacts in combined rolling and normal motion
- Author: M. K. Ghosh
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1986
- Publish Location: [Cleveland, Ohio
“Starvation effects on the hydrodynamic lubrication of rigid nonconformal contacts in combined rolling and normal motion” Subjects and Themes:
- Subjects: ➤ Inlet flow - Lubrication and lubricants - Rigid structures - Rolling moments - Squeeze films - Lubrication - Hydrodynamics - Elastohydrodynamics
Edition Identifiers:
- The Open Library ID: OL16151519M
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 development of an F/A-18 inlet distortion rake: a cost and time saving solution
By Andrew J. Yuhas
“Design and development of an F/A-18 inlet distortion rake: a cost and time saving solution” Metadata:
- Title: ➤ Design and development of an F/A-18 inlet distortion rake: a cost and time saving solution
- Author: Andrew J. Yuhas
- Number of Pages: Median: 19
- Publisher: Dryden Flight Research Center
- Publish Date: 1995
- Publish Location: Edwards, Calif
“Design and development of an F/A-18 inlet distortion rake: a cost and time saving solution” Subjects and Themes:
- Subjects: Inlet flow - F-18 aircraft
Edition Identifiers:
- The Open Library ID: OL22347252M
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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20Turbulence and pressure loss characteristics of the inlet vanes for the 80-by 120-foot wind tunnel
By Michael R. Dudley
“Turbulence and pressure loss characteristics of the inlet vanes for the 80-by 120-foot wind tunnel” Metadata:
- Title: ➤ Turbulence and pressure loss characteristics of the inlet vanes for the 80-by 120-foot wind tunnel
- Author: Michael R. Dudley
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1990
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Turbulence and pressure loss characteristics of the inlet vanes for the 80-by 120-foot wind tunnel” Subjects and Themes:
- Subjects: ➤ Inlet flow - Vanes - Turbulence - Flow characteristics - Wind tunnels - Wind tunnel apparatus - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15405617M
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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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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22User's guide for NASCRIN - a vectorized code for calculating two-dimensional supersonic internal flow fields
By Ajay Kumar
“User's guide for NASCRIN - a vectorized code for calculating two-dimensional supersonic internal flow fields” Metadata:
- Title: ➤ User's guide for NASCRIN - a vectorized code for calculating two-dimensional supersonic internal flow fields
- Author: Ajay Kumar
- Number of Pages: Median: 67
- Publisher: Langley Research Center
- Publish Date: 1984
- Publish Location: Hampton, Va
“User's guide for NASCRIN - a vectorized code for calculating two-dimensional supersonic internal flow fields” Subjects and Themes:
- Subjects: ➤ Euler equations of motion - Inlet flow - Supersonic combustion ramjet engines - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL20986766M
Access and General Info:
- First Year Published: 1984
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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23The effects of vortex ingestion on the flow in a diffusing S-duct
By B. J. Wendt
“The effects of vortex ingestion on the flow in a diffusing S-duct” Metadata:
- Title: ➤ The effects of vortex ingestion on the flow in a diffusing S-duct
- Author: B. J. Wendt
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1994
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“The effects of vortex ingestion on the flow in a diffusing S-duct” Subjects and Themes:
- Subjects: ➤ Inlet flow - Vortices - Cross flow - Vortex generators - Ducted flow - Flow distribution
Edition Identifiers:
- The Open Library ID: OL17000336M
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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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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26Aerodynamic and inlet flow characteristics of several hypersonic airbreathing missile concepts
By James L. Dillon
“Aerodynamic and inlet flow characteristics of several hypersonic airbreathing missile concepts” Metadata:
- Title: ➤ Aerodynamic and inlet flow characteristics of several hypersonic airbreathing missile concepts
- Author: James L. Dillon
- Publisher: AIAA
- Publish Date: 1980
- Publish Location: New York
“Aerodynamic and inlet flow characteristics of several hypersonic airbreathing missile concepts” Subjects and Themes:
- Subjects: Hypersonic missiles - Inlet flow - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL21041827M
Access and General Info:
- First Year Published: 1980
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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27Inlet development for a rocket based combined cycle, single stage to orbit vehicle using computational fluid dynamics
By J. R. DeBonis
“Inlet development for a rocket based combined cycle, single stage to orbit vehicle using computational fluid dynamics” Metadata:
- Title: ➤ Inlet development for a rocket based combined cycle, single stage to orbit vehicle using computational fluid dynamics
- Author: J. R. DeBonis
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: ➤ [Cleveland, Ohio] - [Springfield, Va
“Inlet development for a rocket based combined cycle, single stage to orbit vehicle using computational fluid dynamics” Subjects and Themes:
- Subjects: ➤ Data bases - Databases - Design analysis - Inlet flow - Orbital maneuvers - Reliability analysis - Reynolds averaging - Simulation
Edition Identifiers:
- The Open Library ID: OL15557195M
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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28Development of an experimental data base to validate compressor-face boundary conditions used in unsteady inlet flow computations
By Miklos Sajben
“Development of an experimental data base to validate compressor-face boundary conditions used in unsteady inlet flow computations” Metadata:
- Title: ➤ Development of an experimental data base to validate compressor-face boundary conditions used in unsteady inlet flow computations
- Author: Miklos Sajben
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1998
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Development of an experimental data base to validate compressor-face boundary conditions used in unsteady inlet flow computations” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Inlet flow - Unsteady flow - Boundary conditions - Supersonic inlets - Supersonic compressors
Edition Identifiers:
- The Open Library ID: OL15544614M
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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29Final 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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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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31Effects of inlet conditions on crossflow jet mixing
By D. S. Liscinsky
“Effects of inlet conditions on crossflow jet mixing” Metadata:
- Title: ➤ Effects of inlet conditions on crossflow jet mixing
- Author: D. S. Liscinsky
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Effects of inlet conditions on crossflow jet mixing” Subjects and Themes:
- Subjects: ➤ Mie scattering - Inlet flow - Jet mixing flow - Cross flow - Turbulence effects - Flow distribution
Edition Identifiers:
- The Open Library ID: OL17121316M
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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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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33Computational 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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34Computational modeling and validation for hypersonic inlets
By Louis A. Povinelli
“Computational modeling and validation for hypersonic inlets” Metadata:
- Title: ➤ Computational modeling and validation for hypersonic inlets
- Author: Louis A. Povinelli
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration
- Publish Date: 1990
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Computational modeling and validation for hypersonic inlets” Subjects and Themes:
- Subjects: ➤ Aerodynamics, Hypersonic - Coputational fluid dynamics - Hypersonic Aerodynamics - Hypersonic inlets - Inlet flow - Navier-Stokes equation - Research - Shock wave interaction - Turbulence models
- Places: United States
Edition Identifiers:
- The Open Library ID: OL16127973M
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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35A preliminary design study of supersonic through-flow fan inlets
By Paul J. Barnhart
“A preliminary design study of supersonic through-flow fan inlets” Metadata:
- Title: ➤ A preliminary design study of supersonic through-flow fan inlets
- Author: Paul J. Barnhart
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1988
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“A preliminary design study of supersonic through-flow fan inlets” Subjects and Themes:
- Subjects: ➤ Inlet flow - Aerodynamic drag - Engine design - Turbofan engines - Supersonic flow - Mach number
Edition Identifiers:
- The Open Library ID: OL15407464M
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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36Inlet flow test calibration for a small axial compressor facility
By D. P. Miller
“Inlet flow test calibration for a small axial compressor facility” Metadata:
- Title: ➤ Inlet flow test calibration for a small axial compressor facility
- Author: D. P. Miller
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1994
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Inlet flow test calibration for a small axial compressor facility” Subjects and Themes:
- Subjects: Test facilities - Calibrating - Inlet flow - Turbocompressors - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15404302M
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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37Inlet flow test calibration for a small axial compressor rig
By D. P. Miller
“Inlet flow test calibration for a small axial compressor rig” Metadata:
- Title: ➤ Inlet flow test calibration for a small axial compressor rig
- Author: D. P. Miller
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Inlet flow test calibration for a small axial compressor rig” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Axisymmetric flow - Test stands - Calibrating - Engine testing laboratories - Inlet flow - Turbocompressors
Edition Identifiers:
- The Open Library ID: OL15414468M
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 computational and experimental investigation of a three-dimensional hypersonic scramjet inlet flow field
By Scott Douglas Holland
“A computational and experimental investigation of a three-dimensional hypersonic scramjet inlet flow field” Metadata:
- Title: ➤ A computational and experimental investigation of a three-dimensional hypersonic scramjet inlet flow field
- Author: Scott Douglas Holland
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - North Carolina State University
- Publish Date: 1991
- Publish Location: ➤ Springfield, Va - Raleligh, NC - [Washington, DC
“A computational and experimental investigation of a three-dimensional hypersonic scramjet inlet flow field” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Inlet flow - Supersonic combustion ramjet engines - Three dimensional flow - Hypersonic inlets - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15405796M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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39Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10
By Scott Douglas Holland
“Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10” Metadata:
- Title: ➤ Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10
- Author: Scott Douglas Holland
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center - NASA Center for AeroSpace Information, distributor
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - Hampton, Va - Linthicum Heights, MD
“Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10” Subjects and Themes:
- Subjects: ➤ Inlet flow - Engine design - Hypersonic inlets - Wind tunnel tests - Supersonic combustion ramjet engines - Flow distribution - Hypersonic speed - Internal flow - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15412088M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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40Mach 10 computational study of a three-dimensional scramjet inlet flow field
By Scott Douglas Holland
“Mach 10 computational study of a three-dimensional scramjet inlet flow field” Metadata:
- Title: ➤ Mach 10 computational study of a three-dimensional scramjet inlet flow field
- Author: Scott Douglas Holland
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1995
- Publish Location: Hampton, Va - [Springfield, Va
“Mach 10 computational study of a three-dimensional scramjet inlet flow field” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Inlet flow - Computational grids - Aerodynamics - Three dimensional flow - Supersonic combustion ramjet engines - Navier-Stokes equation - Hypersonic speed - Supersonic inlets - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15410430M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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41Management of total pressure recovery, distortion and high cycle fatigue in compact air vehicle inlets
By Bernhard H. Anderson
“Management of total pressure recovery, distortion and high cycle fatigue in compact air vehicle inlets” Metadata:
- Title: ➤ Management of total pressure recovery, distortion and high cycle fatigue in compact air vehicle inlets
- Author: Bernhard H. Anderson
- 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
“Management of total pressure recovery, distortion and high cycle fatigue in compact air vehicle inlets” Subjects and Themes:
- Subjects: ➤ Inlet flow - Engine design - Pressure recovery - Robutness (Mathematics) - Military aircraft - Statistical analysis
Edition Identifiers:
- The Open Library ID: OL16055644M
Access and General Info:
- First Year Published: 2002
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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42Validation of WIND for a series of inlet flows
By John W. Slater
“Validation of WIND for a series of inlet flows” Metadata:
- Title: ➤ Validation of WIND for a series of inlet flows
- Author: John W. Slater
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - Available from NASA Center for Aerospace Information
- Publish Date: 2002
- Publish Location: ➤ [Cleveland, Ohio] - Hanover, MD
“Validation of WIND for a series of inlet flows” Subjects and Themes:
- Subjects: Computational fluid dynamics - Hypersonic flow - Inlet flow - Subsonic flow - Supersonic flow
Edition Identifiers:
- The Open Library ID: OL16106756M
Access and General Info:
- First Year Published: 2002
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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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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43A 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
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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44A numerical simulation of two-dimensional inlet flow fields
By S. Birignen
“A numerical simulation of two-dimensional inlet flow fields” Metadata:
- Title: ➤ A numerical simulation of two-dimensional inlet flow fields
- Author: S. Birignen
- Publisher: AIAA
- Publish Date: 1981
- Publish Location: New York
“A numerical simulation of two-dimensional inlet flow fields” Subjects and Themes:
- Subjects: Inlet flow
Edition Identifiers:
- The Open Library ID: OL20982643M
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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45Numerical calculation of scramjet inlet flow
By Tomiko Ishiguro
“Numerical calculation of scramjet inlet flow” Metadata:
- Title: ➤ Numerical calculation of scramjet inlet flow
- Author: Tomiko Ishiguro
- Number of Pages: Median: 29
- Publisher: National Aerospace Laboratory
- Publish Date: 1992
- Publish Location: Tokyo, Japan
“Numerical calculation of scramjet inlet flow” Subjects and Themes:
- Subjects: ➤ Inlet flow - Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL19248203M
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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46Study of compressible flow through a rectangular-to-semiannular transition duct
By Jeffry Foster
“Study of compressible flow through a rectangular-to-semiannular transition duct” Metadata:
- Title: ➤ Study of compressible flow through a rectangular-to-semiannular transition duct
- Author: Jeffry Foster
- Number of Pages: Median: 50
- Publisher: Lewis Research Center
- Publish Date: 1995
- Publish Location: Cleveland, Ohio
“Study of compressible flow through a rectangular-to-semiannular transition duct” Subjects and Themes:
- Subjects: Inlet flow - Compressible flow
Edition Identifiers:
- The Open Library ID: OL19002580M
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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47Inlet analysis using computational fluid dynamics
By L. G. Hunter
“Inlet analysis using computational fluid dynamics” Metadata:
- Title: ➤ Inlet analysis using computational fluid dynamics
- Author: L. G. Hunter
- Number of Pages: Median: 10
- Publisher: AIAA
- Publish Date: 1986
- Publish Location: New York
“Inlet analysis using computational fluid dynamics” Subjects and Themes:
- Subjects: Computational fluid dynamics - Inlet flow
Edition Identifiers:
- The Open Library ID: OL18998902M
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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48F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack
By Andrew J. Yuhas
“F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack” Metadata:
- Title: ➤ F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack
- Author: Andrew J. Yuhas
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor]
- Publish Date: 1997
- Publish Location: ➤ Edwards, Calif - [Springfield, Va
“F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack” Subjects and Themes:
- Subjects: ➤ Aircraft maneuvers - Inlet flow - Pressure measurement - Flow characteristics - Angle of attack - Turbofan engines - Research vehicles - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17576171M
- Online Computer Library Center (OCLC) ID: 40617095
Access and General Info:
- First Year Published: 1997
- 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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