Explore: Supersonic Inlets
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Source: The Open Library
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Search results from The Open Library
1A 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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2Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets
By Charles J. Trefny
“Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets” Metadata:
- Title: ➤ Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets
- Author: Charles J. Trefny
- Language: English
- Number of Pages: Median: 60
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Branch - Lewis Research Center
- Publish Date: 1986
- Publish Location: ➤ [Washington, D.C.] - Springfield, Va - Cleveland, Ohio
“Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets” Subjects and Themes:
- Subjects: ➤ Supersonic inlets - Supersonic aircraft - Internal compression inlets - Air intakes - Aerodynamics - Low speed - Jet engines
Edition Identifiers:
- The Open Library ID: OL18218668M - OL19985907M - OL16116660M
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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3Comparison of 3-D viscous flow computations of Mach 5 inlet with experimental data
By D. R. Reddy
“Comparison of 3-D viscous flow computations of Mach 5 inlet with experimental data” Metadata:
- Title: ➤ Comparison of 3-D viscous flow computations of Mach 5 inlet with experimental data
- Author: D. R. Reddy
- Language: English
- Number of Pages: Median: 13
- Publisher: ➤ For sale by the National Technical Information Service - NASA
- Publish Date: 1990
- Publish Location: ➤ [Washington, D.C.] - Springfield, Va
“Comparison of 3-D viscous flow computations of Mach 5 inlet with experimental data” Subjects and Themes:
- Subjects: ➤ Viscous flow - Computational fluid dynamics - Turbulence models - Supersonic inlets - Proving - Navier-Stokes equation - Supersonic wind tunnels - Computer programs
Edition Identifiers:
- The Open Library ID: OL18263195M - OL16138066M - OL17630431M
- Online Computer Library Center (OCLC) ID: 25073883
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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4The effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular duct
By Milo D. Dahl
“The effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular duct” Metadata:
- Title: ➤ The effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular duct
- Author: Milo D. Dahl
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“The effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular duct” Subjects and Themes:
- Subjects: ➤ Duct geometry - Boundary conditions - Supersonic jet flow - Kelvin-Helmholtz instability - Ducted flow - Ducts - Supersonic inlets - Circles (Geometry)
Edition Identifiers:
- The Open Library ID: OL15497499M - OL18118420M - OL17834511M
- Online Computer Library Center (OCLC) ID: 39722385
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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5Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
By Masashi Mizukami
“Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Metadata:
- Title: ➤ Parametrics on 2D 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]
“Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Inviscid flow - Supersonic diffusers - Computational grids - Two dimensional flow - Turbulence models - Navier-Stokes equation - Supersonic inlets
Edition Identifiers:
- The Open Library ID: OL15414474M - OL17116401M - OL18081585M
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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6Computation of multi-dimensional viscous supersonic jet flow
By Y. N. Kim
“Computation of multi-dimensional viscous supersonic jet flow” Metadata:
- Title: ➤ Computation of multi-dimensional viscous supersonic jet flow
- Author: Y. N. Kim
- Language: English
- Number of Pages: Median: 124
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - Lewis Research Center - For sale by the National Technical Information Service
- Publish Date: 1986
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.] - Cleveland, Ohio
“Computation of multi-dimensional viscous supersonic jet flow” Subjects and Themes:
- Subjects: ➤ Intake systems - Computational fluid dynamics - Fluid dynamics - Jet flow - Supersonic flow - Three dimensional flow - Navier-Stokes equations - Jets - Two dimensional flow - Viscous flow - Supersonic inlets - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL20985136M - OL15415474M - OL18082302M
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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7An 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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8Comparison 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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9Numerical 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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10Validation of the RPLUS3D code for supersonic inlet applications involving three-dimensional shock wave boundary layer interactions
By Kamlesh Kapoor
“Validation of the RPLUS3D code for supersonic inlet applications involving three-dimensional shock wave boundary layer interactions” Metadata:
- Title: ➤ Validation of the RPLUS3D code for supersonic inlet applications involving three-dimensional shock wave boundary layer interactions
- 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]
“Validation of the RPLUS3D code for supersonic inlet applications involving three-dimensional shock wave boundary layer interactions” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Computer programs - Finite volume method - Flat plates - Laminar boundary layer - Navier-Stokes equation - Shock wave interaction - Supersonic inlets - Three dimensional boundary layer - Three dimensional models - Turbulent boundary layer - Wedges
Edition Identifiers:
- The Open Library ID: OL15402776M - OL17790154M
- Online Computer Library Center (OCLC) ID: 32158036
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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11On supersonic-inlet boundary-layer bleed flow
By G. J. Harloff
“On supersonic-inlet boundary-layer bleed flow” Metadata:
- Title: ➤ On supersonic-inlet boundary-layer bleed flow
- Author: G. J. Harloff
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“On supersonic-inlet boundary-layer bleed flow” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Bleeding - Mathematical models - Boundary conditions - Boundary layer flow - Boundary layer control - Compressible flow - Supersonic inlets
Edition Identifiers:
- The Open Library ID: OL15409168M - OL18078927M
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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12Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients
By Bobby W. Sanders
“Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients” Metadata:
- Title: ➤ Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients
- Author: Bobby W. Sanders
- Language: English
- Number of Pages: Median: 98
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1980
- Publish Location: Washington, D.C
“Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients” Subjects and Themes:
- Subjects: ➤ Airplanes - Turbojet engines - Air intakes - Motors - Valves - Aerodynamic stability - Bypasses - Propulsion system performance - Supersonic inlets - Wind tunnel stability tests
Edition Identifiers:
- The Open Library ID: OL43506459M
- Online Computer Library Center (OCLC) ID: 761221787
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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13Minimum weight design of a generic axisymmetric inlet
By Shari-Beth Nadell
“Minimum weight design of a generic axisymmetric inlet” Metadata:
- Title: ➤ Minimum weight design of a generic axisymmetric inlet
- Author: Shari-Beth Nadell
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Minimum weight design of a generic axisymmetric inlet” Subjects and Themes:
- Subjects: ➤ Engine design - Symmetry - Supersonic inlets - Air intakes - Structural weight - Structural design - Finite element method
Edition Identifiers:
- The Open Library ID: OL15497406M
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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14The use of a lidar forward-looking turbulence sensor for mixed-compression inlet unstart avoidance and gross weight reduction on a high speed civil transport
By David Soreide
“The use of a lidar forward-looking turbulence sensor for mixed-compression inlet unstart avoidance and gross weight reduction on a high speed civil transport” Metadata:
- Title: ➤ The use of a lidar forward-looking turbulence sensor for mixed-compression inlet unstart avoidance and gross weight reduction on a high speed civil transport
- Author: David Soreide
- 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
“The use of a lidar forward-looking turbulence sensor for mixed-compression inlet unstart avoidance and gross weight reduction on a high speed civil transport” Subjects and Themes:
- Subjects: ➤ Supersonic inlets - Warning systems - Atmospheric turbulence - Commercial aircraft - Airborne equipment - Flight instruments - Optical radar - Supersonic transports
Edition Identifiers:
- The Open Library ID: OL15550562M
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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15A method for generating reduced-order linear models of multidimensional supersonic inlets
By Amy Chicatelli
“A method for generating reduced-order linear models of multidimensional supersonic inlets” Metadata:
- Title: ➤ A method for generating reduced-order linear models of multidimensional supersonic inlets
- Author: Amy Chicatelli
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1998
- Publish Location: ➤ [Cleveland, Ohio] - [Springfield, Va
“A method for generating reduced-order linear models of multidimensional supersonic inlets” Subjects and Themes:
- Subjects: Computational fluid dynamics - Supersonic inlets - Propulsion system performance - Computerized simulation - Propulsion system configurations
Edition Identifiers:
- The Open Library ID: OL15544573M
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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16A method for generating reduced order linear models of supersonic inlets
By Amy Chicatelli
“A method for generating reduced order linear models of supersonic inlets” Metadata:
- Title: ➤ A method for generating reduced order linear models of supersonic inlets
- Author: Amy Chicatelli
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, DC - Springfield, Va
“A method for generating reduced order linear models of supersonic inlets” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Matrices (Mathematics) - Supersonic inlets - Linearization - Linear equations - Computerized simulation
Edition Identifiers:
- The Open Library ID: OL15505229M
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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17Development 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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18Random-choice-method solutions for two-dimensional planar and axisymmetric steady supersonic flows
By Z. C. Shi
“Random-choice-method solutions for two-dimensional planar and axisymmetric steady supersonic flows” Metadata:
- Title: ➤ Random-choice-method solutions for two-dimensional planar and axisymmetric steady supersonic flows
- Author: Z. C. Shi
- Number of Pages: Median: 39
- Publisher: ➤ Institute for Aerospace Studies
- Publish Date: 1986
- Publish Location: [Downsview, Ont.]
“Random-choice-method solutions for two-dimensional planar and axisymmetric steady supersonic flows” Subjects and Themes:
- Subjects: Steady flow - Supersonic flow - Free jets - Supersonic nozzles - Supersonic inlets
Edition Identifiers:
- The Open Library ID: OL19985858M
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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19Mach 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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20Verification assessment of flow boundary conditions for CFD analysis of supersonic inlet flows
By John W. Slater
“Verification assessment of flow boundary conditions for CFD analysis of supersonic inlet flows” Metadata:
- Title: ➤ Verification assessment of flow boundary conditions for CFD analysis of supersonic inlet flows
- Author: John W. Slater
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2002
- Publish Location: Cleveland, Ohio
“Verification assessment of flow boundary conditions for CFD analysis of supersonic inlet flows” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL16098750M
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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21Numerical simulation of supersonic flow using a new analytical bleed boundary condition
By G. J. Harloff
“Numerical simulation of supersonic flow using a new analytical bleed boundary condition” Metadata:
- Title: ➤ Numerical simulation of supersonic flow using a new analytical bleed boundary condition
- Author: G. J. Harloff
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Numerical simulation of supersonic flow using a new analytical bleed boundary condition” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Supersonic boundary layers - Supersonic flow - Flow distribution - Oblique shock waves - Boundary layer control - Supersonic inlets - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15381444M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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22A comparison of approximate methods of predicting shock detachment distance for two-dimensional supersonic inlets
By Harry E. Schulte
“A comparison of approximate methods of predicting shock detachment distance for two-dimensional supersonic inlets” Metadata:
- Title: ➤ A comparison of approximate methods of predicting shock detachment distance for two-dimensional supersonic inlets
- Author: Harry E. Schulte
- Number of Pages: Median: 47
- Publisher: ➤ Faculty of the School of Engineering, Air Force Institute of Technology, Air University
- Publish Date: 1974
- Publish Location: ➤ Wright-Patterson Air Force Base, Ohio
“A comparison of approximate methods of predicting shock detachment distance for two-dimensional supersonic inlets” Subjects and Themes:
- Subjects: Drag - Shock waves - Bow waves - Supersonic inlets
Edition Identifiers:
- The Open Library ID: OL20986757M
Access and General Info:
- First Year Published: 1974
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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23Internal performance of a variable ramp mixed compression intake at Mach 3.05
By S. A. Fisher
“Internal performance of a variable ramp mixed compression intake at Mach 3.05” Metadata:
- Title: ➤ Internal performance of a variable ramp mixed compression intake at Mach 3.05
- Author: S. A. Fisher
- Number of Pages: Median: 10
- Publisher: ➤ Aeronautical Research Laboratories
- Publish Date: 1985
- Publish Location: Melbourne, Vic
“Internal performance of a variable ramp mixed compression intake at Mach 3.05” Subjects and Themes:
- Subjects: Air intakes - Boundary layer control - Supersonic inlets
Edition Identifiers:
- The Open Library ID: OL19985969M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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24Analysis of inlet-compressor acoustic interactions using coupled CFD codes
By A. Suresh
“Analysis of inlet-compressor acoustic interactions using coupled CFD codes” Metadata:
- Title: ➤ Analysis of inlet-compressor acoustic interactions using coupled CFD codes
- Author: A. Suresh
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ [Springfield, Va - [Cleveland, Ohio]
“Analysis of inlet-compressor acoustic interactions using coupled CFD codes” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL17581867M
- Online Computer Library Center (OCLC) ID: 41519876
Access and General Info:
- First Year Published: 1998
- 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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25Joint US/Russia TU-144 engine ground tests
“Joint US/Russia TU-144 engine ground tests” Metadata:
- Title: ➤ Joint US/Russia TU-144 engine ground tests
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Joint US/Russia TU-144 engine ground tests” Subjects and Themes:
- Subjects: ➤ Engine tests - Aircraft engines - TU-144 aircraft - Supersonic inlets - Flow characteristics - Supersonic transport
Edition Identifiers:
- The Open Library ID: OL17579566M
- Online Computer Library Center (OCLC) ID: 41105988
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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Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Diverterless supersonic inlet
A diverterless supersonic inlet (DSI) is a type of jet engine air intake used by some modern combat aircraft to control air flow into their engines. It
Components of jet engines
org "How supersonic inlets work" J. Thomas Anderson Fig1 enginehistory.org "How supersonic inlets work" J. Thomas Anderson Section 5.2 "Inlet operating
Inlet cone
use an inlet cone. The inlet cone for circular/axisymmetric inlets has its equivalent in the intake ramp for 2-D/rectangular inlets. An inlet cone, as
Sonic boom
crack of a supersonic bullet passing overhead or the crack of a bullwhip are examples of a small sonic boom. Sonic booms due to large supersonic aircraft
Shenyang J-35
and engine blades are hidden by the serpentine inlets (S-ducts) behind the diverterless supersonic inlets (DSI) bumps, which obscure the reflective surface
Chengdu J-36
dual-wheel nose landing gear, two under-wing caret inlets, one dorsal intake with diverterless supersonic inlet, double delta wings with one leading-edge extension
Concorde
Concorde (/ˈkɒŋkɔːd/) is a retired Anglo-French supersonic airliner jointly developed and manufactured by Sud Aviation and the British Aircraft Corporation
Lockheed SR-71 Blackbird
Anderson, J. Thomas (2013). How Supersonic Inlets Work – Details of the Geometry and Operation of the SR-71 Mixed Compression Inlet. AEHS convention. Engine
Intake ramp
designed to generate a number of shock waves to aid the inlet compression process at supersonic speeds; such intakes are also referred to as two dimensional
Chengdu J-20
mature design similar to the F-22. The diverterless supersonic inlets (DSI) leading into serpentine inlets (S-ducts) can obscure the reflective surface of