Explore: Supersonic Flow
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Source: The Open Library
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Search results from The Open Library
1A two-dimensional numerical simulation of a supersonic, chemically reacting mixing layer
By J. Philip Drummond
“A two-dimensional numerical simulation of a supersonic, chemically reacting mixing layer” Metadata:
- Title: ➤ A two-dimensional numerical simulation of a supersonic, chemically reacting mixing layer
- Author: J. Philip Drummond
- Language: English
- Number of Pages: Median: 100
- Publisher: ➤ Langley Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Division - For sale by the National Technical Information Service]
- Publish Date: 1988 - 1989
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, DC]
“A two-dimensional numerical simulation of a supersonic, chemically reacting mixing layer” Subjects and Themes:
- Subjects: Fluid mechanics - Supersonic flow - Mixing layers
Edition Identifiers:
- The Open Library ID: OL18028939M - OL17095800M - OL14664085M - OL18928581M - OL15274898M
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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2Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle
By Stephen W. D. Wolf
“Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle” Metadata:
- Title: ➤ Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle
- Author: Stephen W. D. Wolf
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - MCAT Institute - National Technical Information Service, distributor
- Publish Date: 1991 - 1992 - 1993 - 1995
- Publish Location: ➤ San Jose, CA - Springfield, Va.? - [Washington, DC - [Washington, D.C - Springfield, Va
“Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle” Subjects and Themes:
- Subjects: ➤ Supersonic wind tunnels - Supersonic nozzles - Nozzle design - Flow measurement - Supersonic flow - Swept wings - Wind tunnel apparatus - Design and construction - Laminar flow - Boundary layer transition - Flow distribution - Cryogenics
Edition Identifiers:
- The Open Library ID: OL15387214M - OL15419085M - OL14684284M - OL14700996M
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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3Methodology for sensitivity analysis, approximate analysis, and design optimization in CFD for multidisciplinary applications
By Arthur C. Taylor
“Methodology for sensitivity analysis, approximate analysis, and design optimization in CFD for multidisciplinary applications” Metadata:
- Title: ➤ Methodology for sensitivity analysis, approximate analysis, and design optimization in CFD for multidisciplinary applications
- Author: Arthur C. Taylor
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Old Dominion University Research Foundation - Dept. of Mechanical Engineering, College of Engineering & Technology, Old Dominion University
- Publish Date: 1992 - 1993 - 1994 - 1996
- Publish Location: ➤ Norfolk, Va - Springfield, Va - [Washington, DC - [Springfield, Va - [Washington, D.C
“Methodology for sensitivity analysis, approximate analysis, and design optimization in CFD for multidisciplinary applications” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Airfoils - Algorithms - Architecture (Computers) - Computational fluid dynamics - Design analysis - Iterative solution - Linear equations - Matrices (Mathematics) - Memory (Computers) - Navier-Stokes equation - Optimization - Sensitivity - Software tools - Supersonic flow - Turbulent flows - Viscous flow
Edition Identifiers:
- The Open Library ID: OL15359487M - OL17030214M - OL15402708M - OL15498963M
- Online Computer Library Center (OCLC) ID: 32752276
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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4F-16XL-2 supersonic laminar flow control flight test experiment
By Scott G. Anders
“F-16XL-2 supersonic laminar flow control flight test experiment” Metadata:
- Title: ➤ F-16XL-2 supersonic laminar flow control flight test experiment
- Author: Scott G. Anders
- Language: English
- Publisher: ➤ National Technical Information Service [distributor - National Aeronautics and Space Administration, Langley Research Center - Available from NASA Center for AeroSpace Information
- Publish Date: 1999
- Publish Location: ➤ Hampton, Va - Springfield, VA - Hanover, MD
“F-16XL-2 supersonic laminar flow control flight test experiment” Subjects and Themes:
- Subjects: Computational fluid dynamics - Supersonic flow - Boundary layer control - Laminar flow - Design analysis
Edition Identifiers:
- The Open Library ID: OL18140131M - OL17595528M - OL15569345M - OL18296124M
- Online Computer Library Center (OCLC) ID: 44442105
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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5The effect of three-dimensional freestream disturbances on the supersonic flow past a wedge
By Peter W. Duck
“The effect of three-dimensional freestream disturbances on the supersonic flow past a wedge” Metadata:
- Title: ➤ The effect of three-dimensional freestream disturbances on the supersonic flow past a wedge
- Author: Peter W. Duck
- Language: English
- Publisher: ➤ Institute for Computer Applications in Science and Engineering, NASA Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: [Springfield, Va - Hampton, VA
“The effect of three-dimensional freestream disturbances on the supersonic flow past a wedge” Subjects and Themes:
- Subjects: ➤ Supersonic flow - Free flow - Uniform flow - Aerodynamic stability - Aerodynamic characteristics - Wedges - Fourier series - Shock waves
Edition Identifiers:
- The Open Library ID: OL17564669M - OL15485941M - OL18114303M - OL17123820M
- Online Computer Library Center (OCLC) ID: 39284442
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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6Application of a two-dimensional unsteady viscous analysis code to a supersonic throughflow fan stage
By Ronald J. Steinke
“Application of a two-dimensional unsteady viscous analysis code to a supersonic throughflow fan stage” Metadata:
- Title: ➤ Application of a two-dimensional unsteady viscous analysis code to a supersonic throughflow fan stage
- Author: Ronald J. Steinke
- Language: English
- Number of Pages: Median: 14
- Publisher: ➤ Lewis Research Center - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service]
- Publish Date: 1989
- Publish Location: ➤ Cleveland, Ohio - [Springfield, Va - [Washington, D.C.]
“Application of a two-dimensional unsteady viscous analysis code to a supersonic throughflow fan stage” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Aerodynamics, Supersonic - Computer programs - Computer simulation - Design and construction - Rotor blades - Supersonic Aerodynamics - Supersonic flow - Turbomachinery - Turbomachines - Unsteady flow - Unsteady flow (Aerodynamics) - Viscous flow
Edition Identifiers:
- The Open Library ID: OL16138023M - OL19380256M - OL18263181M - OL17630288M
- Online Computer Library Center (OCLC) ID: 24900111
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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7A multi-domain spectral method for supersonic reactive flows
By Wai-Sun Don
“A multi-domain spectral method for supersonic reactive flows” Metadata:
- Title: ➤ A multi-domain spectral method for supersonic reactive flows
- Author: Wai-Sun Don
- Language: English
- Number of Pages: Median: 24
- Publisher: ➤ National Technical Information Service, distributor - Institute for Computer Applications in Science and Engineering, National Aeronautics and Space Administration, Langley Research Center - Institute for Computer Applications in Science and Engineering, NASA Langley Research Center - For sale by the National Technical Information Service
- Publish Date: 2002
- Publish Location: ➤ Hampton, VA - Hampton, Va - Springfield, VA - [Springfield, Va
“A multi-domain spectral method for supersonic reactive flows” Subjects and Themes:
- Subjects: ➤ Aerodynamics, Supersonic - Chebyshev approximation - Computerized simulation - Flow distribution - Mathematical models - Reacting flow - Spectral methods - Spectral theory (Mathematics) - Supersonic Aerodynamics - Supersonic flow
Edition Identifiers:
- The Open Library ID: OL16125369M - OL18227528M - OL21495158M - OL17633141M
- Online Computer Library Center (OCLC) ID: 60338513
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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8Numerical simulation of shock/turbulent boundary layer interaction
By Sedat Biringen
“Numerical simulation of shock/turbulent boundary layer interaction” Metadata:
- Title: ➤ Numerical simulation of shock/turbulent boundary layer interaction
- Author: Sedat Biringen
- Language: English
- Publisher: ➤ Dept. of Aerospace Engineering Sciences, University of Colorado - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1993
- Publish Location: ➤ [Washington, D.C - Boulder, Colo - Springfield, Va
“Numerical simulation of shock/turbulent boundary layer interaction” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Turbulent flow - Turbulent boundary layer - Three dimensional models - Computerized simulation - Compressible boundary layer - Finite difference theory - Compressibility effects - Shock wave interaction - Energy transfer - Compressible flow - Nonlinear equations - Navier-Stokes equation - Supersonic flow - Shock waves
Edition Identifiers:
- The Open Library ID: OL17792155M - OL17684090M - OL18081888M
- Online Computer Library Center (OCLC) ID: 33958147
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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9In-flight imaging of transverse gas jets injected into transonic and supersonic crossflows
By Kon-Sheng Charles Wang
“In-flight imaging of transverse gas jets injected into transonic and supersonic crossflows” Metadata:
- Title: ➤ In-flight imaging of transverse gas jets injected into transonic and supersonic crossflows
- Author: Kon-Sheng Charles Wang
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility - National Technical Information Service, distributor]
- Publish Date: 1994
- Publish Location: ➤ Edwards, Calif - [Springfield, Va
“In-flight imaging of transverse gas jets injected into transonic and supersonic crossflows” Subjects and Themes:
- Subjects: ➤ Cross flow - Flight test vehicles - Flow visualization - Gas injection - Hypersonic flow - Imaging techniques - Supersonic flow
Edition Identifiers:
- The Open Library ID: OL15408546M - OL18078619M - OL17005135M
- Online Computer Library Center (OCLC) ID: 32668590
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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10Computation of Navier-Stokes equations for three-dimensional flow separation
By Ching-Mao Hung
“Computation of Navier-Stokes equations for three-dimensional flow separation” Metadata:
- Title: ➤ Computation of Navier-Stokes equations for three-dimensional flow separation
- Author: Ching-Mao Hung
- Language: English
- Number of Pages: Median: 19
- 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
“Computation of Navier-Stokes equations for three-dimensional flow separation” Subjects and Themes:
- Subjects: ➤ Fluid dynamics - Mathematical models - Computational fluid dynamics - Flat plates - Boundary layer separation - Supersonic flow - Flow distribution
Edition Identifiers:
- The Open Library ID: OL18263481M - OL17630346M - OL16138491M
- Online Computer Library Center (OCLC) ID: 25291040
Author's Alternative Names:
"Ching-mao Hung"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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11Supersonic wing and wing-body shape optimization using an adjoint formulation
By James Reuther
“Supersonic wing and wing-body shape optimization using an adjoint formulation” Metadata:
- Title: ➤ Supersonic wing and wing-body shape optimization using an adjoint formulation
- Author: James Reuther
- Language: English
- Publisher: ➤ Research Institute for Advanced Computer Science, NASA Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Moffett Field, Calif.]
“Supersonic wing and wing-body shape optimization using an adjoint formulation” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Supersonic aircraft - Body-wing configurations - Supersonic flow - Three dimensional flow - Control theory - Optimization - Euler equations of motion - Aerodynamic configurations - Aircraft design - Wings - Supersonic airfoils
Edition Identifiers:
- The Open Library ID: OL18084750M - OL15419682M - OL17076145M
- Online Computer Library Center (OCLC) ID: 34762339
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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12Supersonic laminar flow control research
By Ching F. Lo
“Supersonic laminar flow control research” Metadata:
- Title: ➤ Supersonic laminar flow control research
- Author: Ching F. Lo
- Language: English
- Publisher: ➤ Ames Research Center - National Aeronautics and Space Administration - University of Tennessee, Space Institute - National Technical Information Service, distributor
- Publish Date: 1995 - 1996
- Publish Location: ➤ Tullahoma, TN - [Springfield, Va - Moffett Field, CA - [Washington, DC - Springfield, Va
“Supersonic laminar flow control research” Subjects and Themes:
- Subjects: ➤ Boundary layer stability - Supersonic boundary layers - Boundary layer control - Supersonic flow - Laminar flow - Active control - Computational fluid dynamics - Control systems design - Boundary layer flow - Laminar boundary layer - Boundary layer transition - Wind tunnel nozzles - Stability - Temperature distribution - Wind tunnel tests - Laminar boundary - Wall temperature - Supersonic wind tunnels - Prediction analysis techniques - Nozzle design
Edition Identifiers:
- The Open Library ID: OL15543412M - OL15424662M - OL15506457M
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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13Wing-section optimization for supersonic viscous flow
By Cem C. Item
“Wing-section optimization for supersonic viscous flow” Metadata:
- Title: ➤ Wing-section optimization for supersonic viscous flow
- Author: Cem C. Item
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Wing-section optimization for supersonic viscous flow” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Viscous flow - Mathematical models - Supersonic flow - Aicraft design - Navier-Stokes equation - Airfoils - Aerodynamic configurations - Two dimensional models - Computer aided design
Edition Identifiers:
- The Open Library ID: OL17078554M - OL18084623M - OL15419484M
- Online Computer Library Center (OCLC) ID: 34608891
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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14Computation 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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15Embedded function methods for compressible high speed turbulent flow
By J. D. A. Walker
“Embedded function methods for compressible high speed turbulent flow” Metadata:
- Title: ➤ Embedded function methods for compressible high speed turbulent flow
- Author: J. D. A. Walker
- Language: English
- Publisher: NASA Langley Research Center
- Publish Date: 1994
- Publish Location: Hampton, Va
“Embedded function methods for compressible high speed turbulent flow” Subjects and Themes:
- Subjects: ➤ Compressible flow - Computational fluid dynamics - Supersonic boundary layers - Supersonic flow - Turbulent boundary layer - Turbulent flow
Edition Identifiers:
- The Open Library ID: OL17790660M - OL15408583M
- Online Computer Library Center (OCLC) ID: 32668807
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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16The behaviour of free molecule cylindrical Langmuir probes in supersonic flows, and their application to the study of the blunt body stagnation layer
By A. A. Sonin
“The behaviour of free molecule cylindrical Langmuir probes in supersonic flows, and their application to the study of the blunt body stagnation layer” Metadata:
- Title: ➤ The behaviour of free molecule cylindrical Langmuir probes in supersonic flows, and their application to the study of the blunt body stagnation layer
- Author: A. A. Sonin
- Number of Pages: Median: 64
- Publisher: ➤ Institute for Aerospace Studies - [Institute for Aerospace Studies]
- Publish Date: 1965
- Publish Location: [Downsview, Ont.]
“The behaviour of free molecule cylindrical Langmuir probes in supersonic flows, and their application to the study of the blunt body stagnation layer” Subjects and Themes:
- Subjects: Electrostatic probes - Supersonic flow
Edition Identifiers:
- The Open Library ID: OL20897792M - OL20986454M
Access and General Info:
- First Year Published: 1965
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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17Flow characteristics in boundary layer bleed slots with plenum
By A. Hamed
“Flow characteristics in boundary layer bleed slots with plenum” Metadata:
- Title: ➤ Flow characteristics in boundary layer bleed slots with plenum
- Author: A. Hamed
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - For sale by the National Technical Information Service
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“Flow characteristics in boundary layer bleed slots with plenum” Subjects and Themes:
- Subjects: ➤ Boundary layer control - Boundary layer flow - Flow characteristics - Oblique shock waves - Plenum chambers - Pressure gradients - Shock wave interaction - Slots - Supersonic flow - Turbulent boundary layer
Edition Identifiers:
- The Open Library ID: OL17793989M - OL15419025M
- Online Computer Library Center (OCLC) ID: 34757915
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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18STARS
By Kajal K. Gupta
“STARS” Metadata:
- Title: STARS
- Author: Kajal K. Gupta
- Language: English
- Number of Pages: Median: 160
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility - For sale by the National Technical Information Service
- Publish Date: 1990 - 1991
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“STARS” Subjects and Themes:
- Subjects: ➤ Aerodynamic forces - Aeroelasticity - Aeroservoelasticity - Computer programs - Control stability - Finite element method - Structural analysis - Structural analysis (Engineering) - Subsonic flow - Supersonic flow - Unsteady aerodynamics
Edition Identifiers:
- The Open Library ID: OL16131038M - OL16132316M
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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19Special course on shock-wave/boundary-layer interactions in supersonic and hypersonic flows
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
“Special course on shock-wave/boundary-layer interactions in supersonic and hypersonic flows” Metadata:
- Title: ➤ Special course on shock-wave/boundary-layer interactions in supersonic and hypersonic flows
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
- Language: English
- Number of Pages: Median: 298
- Publisher: AGARD
- Publish Date: 1993
- Publish Location: ➤ Neuilly-sur-Seine - Neuilly-sur-Seine, France
“Special course on shock-wave/boundary-layer interactions in supersonic and hypersonic flows” Subjects and Themes:
- Subjects: ➤ Hypersonic flow - Shock-boundary layer interaction - Supersonic flow
Edition Identifiers:
- The Open Library ID: OL20259070M - OL19917512M
- All ISBNs: 9789283507185 - 9283507185
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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20Special course on three-dimensional supersonic/hypersonic flows including separation
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
“Special course on three-dimensional supersonic/hypersonic flows including separation” Metadata:
- Title: ➤ Special course on three-dimensional supersonic/hypersonic flows including separation
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
- Language: English
- Number of Pages: Median: 394
- Publisher: AGARD
- Publish Date: 1990
- Publish Location: ➤ Neuilly-sur-Seine - Neuilly sur Seine, France
“Special course on three-dimensional supersonic/hypersonic flows including separation” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL20124782M - OL21039442M
- All ISBNs: 9789283505372 - 9283505379
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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21An edge-based solution-adaptive method applied to the AIRPLANE code
By Rupak Biswas
“An edge-based solution-adaptive method applied to the AIRPLANE code” Metadata:
- Title: ➤ An edge-based solution-adaptive method applied to the AIRPLANE code
- Author: Rupak Biswas
- Language: English
- Publisher: ➤ Research Institute for Advanced Computer Science, NASA Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Moffett Field, CA]
“An edge-based solution-adaptive method applied to the AIRPLANE code” Subjects and Themes:
- Subjects: ➤ Pressure distribution - Transonic flow - Near fields - Unstructured grids (Mathematics) - Flow distribution - Aircraft configurations - Sonic booms - Grid generation (Mathematics) - Supersonic flow - Shock waves
Edition Identifiers:
- The Open Library ID: OL15419501M - OL18084638M
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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22A numerical method for solving the three-dimensional parabolized Navier-Stokes equations
By Domenic D'Ambrosio
“A numerical method for solving the three-dimensional parabolized Navier-Stokes equations” Metadata:
- Title: ➤ A numerical method for solving the three-dimensional parabolized Navier-Stokes equations
- Author: Domenic D'Ambrosio
- Language: English
- Publisher: ➤ Institute for Computer Applications in Science and Engineering, NASA Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: Hampton, VA - [Springfield, Va
“A numerical method for solving the three-dimensional parabolized Navier-Stokes equations” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Corner flow - Essentially non-oscillatory schemes - Flux difference splitting - Inviscid flow - Navier-Stokes equation - Supersonic flow - Three dimensional flow - Viscous flow
Edition Identifiers:
- The Open Library ID: OL17791703M - OL15413863M
- Online Computer Library Center (OCLC) ID: 34061925
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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23The Kirchhoff formulas for moving surfaces in aeroacoustics
By F. Farassat
“The Kirchhoff formulas for moving surfaces in aeroacoustics” Metadata:
- Title: ➤ The Kirchhoff formulas for moving surfaces in aeroacoustics
- Author: F. Farassat
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: Hampton, Va - [Springfield, Va
“The Kirchhoff formulas for moving surfaces in aeroacoustics” Subjects and Themes:
- Subjects: ➤ Kirchhoff law - Aeroacoustics - Noise prediction - Supersonic flow - Electromagnetism - Subsonic speed - Pipe flow
Edition Identifiers:
- The Open Library ID: OL17807035M - OL15482768M
- Online Computer Library Center (OCLC) ID: 37955730
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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24Computation of asymmetric supersonic flows around cones at large incidence
By David Degani
“Computation of asymmetric supersonic flows around cones at large incidence” Metadata:
- Title: ➤ Computation of asymmetric supersonic flows around cones at large incidence
- Author: David Degani
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - Technion Research & Development Foundation
- Publish Date: 1987
- Publish Location: ➤ Springfield, Va - Technion City, Haifa, Israel - [Washington, D.C
“Computation of asymmetric supersonic flows around cones at large incidence” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Flow equations - Vortices - Supersonic flow - Conical bodies - Navier-Stokes equation - Spatial marching - Conical flow - Angle of attack
Edition Identifiers:
- The Open Library ID: OL17683849M - OL14980900M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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25An extended Lagrangian method
By Meng-Sing Liou
“An extended Lagrangian method” Metadata:
- Title: An extended Lagrangian method
- Author: Meng-Sing Liou
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1992 - 1995
- Publish Location: ➤ Springfield, Va - [Washington, D.C - [Washington, DC
“An extended Lagrangian method” Subjects and Themes:
- Subjects: ➤ Unsteady flow - Computational grids - Supersonic flow - Subsonic flow - Lagrange equations - Lagrangian function
Edition Identifiers:
- The Open Library ID: OL14698842M - OL15498355M
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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26Boundary layer measurements in the UTIA 5 - by 7 - inch supersonic wind tunnel
By J. Ruptash
“Boundary layer measurements in the UTIA 5 - by 7 - inch supersonic wind tunnel” Metadata:
- Title: ➤ Boundary layer measurements in the UTIA 5 - by 7 - inch supersonic wind tunnel
- Author: J. Ruptash
- Number of Pages: Median: 23
- Publisher: ➤ Institute of Aerophysics - [Institute of Aerophysics]
- Publish Date: 1952
- Publish Location: [Downsview, Ont.]
“Boundary layer measurements in the UTIA 5 - by 7 - inch supersonic wind tunnel” Subjects and Themes:
- Subjects: Supersonic flow - Turbulent boundary layer
Edition Identifiers:
- The Open Library ID: OL20897506M - OL19986920M
Access and General Info:
- First Year Published: 1952
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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27Nonlinear interaction between a pair of oblique modes in a supersonic mixing layer
By Thomas F. Balsa
“Nonlinear interaction between a pair of oblique modes in a supersonic mixing layer” Metadata:
- Title: ➤ Nonlinear interaction between a pair of oblique modes in a supersonic mixing layer
- Author: Thomas F. Balsa
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Nonlinear interaction between a pair of oblique modes in a supersonic mixing layer” Subjects and Themes:
- Subjects: ➤ Base flow - Flow stability - Interactional aerodynamics - Mixing layers (Fluids) - Shear flow - Supersonic flow - Vortex sheets
Edition Identifiers:
- The Open Library ID: OL15411630M - OL17790780M
- Online Computer Library Center (OCLC) ID: 32920327
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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28Instrumentation development for study of Reynolds analogy in reacting flows
By Dianne J. DeTurris
“Instrumentation development for study of Reynolds analogy in reacting flows” Metadata:
- Title: ➤ Instrumentation development for study of Reynolds analogy in reacting flows
- Author: Dianne J. DeTurris
- 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
“Instrumentation development for study of Reynolds analogy in reacting flows” Subjects and Themes:
- Subjects: ➤ Friction measurement - Heat transfer - Reacting flow - Skin friction - Strain gages - Supersonic combustion - Supersonic combustion ramjet engines - Supersonic flow - Turbulent boundary layer - Wall flow
Edition Identifiers:
- The Open Library ID: OL15421527M - OL17793730M
- Online Computer Library Center (OCLC) ID: 35218955
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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29Seeding for laser velocimetry in confined supersonic flows with shocks
By J. Lepicovsky
“Seeding for laser velocimetry in confined supersonic flows with shocks” Metadata:
- Title: ➤ Seeding for laser velocimetry in confined supersonic flows with shocks
- Author: J. Lepicovsky
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Seeding for laser velocimetry in confined supersonic flows with shocks” Subjects and Themes:
- Subjects: Laser Doppler velocimeters - Optical measuring instruments - Reliability - Supersonic flow - Velocity measurement
Edition Identifiers:
- The Open Library ID: OL15496502M - OL17834532M
- Online Computer Library Center (OCLC) ID: 39668684
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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30Wing-section optimization for supersonic viscous flows
By Cem C. Item
“Wing-section optimization for supersonic viscous flows” Metadata:
- Title: ➤ Wing-section optimization for supersonic viscous flows
- Author: Cem C. Item
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Wing-section optimization for supersonic viscous flows” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Aerodynamic configurations - Aicraft design - Airfoils - Applications programs (Computers) - Computational fluid dynamics - Inviscid flow - Navier-Stokes equation - Optimization - Supersonic flow - Viscous flow
Edition Identifiers:
- The Open Library ID: OL18084626M - OL17078549M
- Online Computer Library Center (OCLC) ID: 34609263
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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31Supersonic flow in a shock tube of divergent cross-section
By Edwin K. Parks
“Supersonic flow in a shock tube of divergent cross-section” Metadata:
- Title: ➤ Supersonic flow in a shock tube of divergent cross-section
- Author: Edwin K. Parks
- Number of Pages: Median: 31
- Publisher: ➤ Institute of Aerophysics - [Institute of Aerophysics]
- Publish Date: 1952
- Publish Location: [Downsview, Ont.]
“Supersonic flow in a shock tube of divergent cross-section” Subjects and Themes:
- Subjects: Supersonic flow - Diffraction - Shock waves
Edition Identifiers:
- The Open Library ID: OL19986924M - OL20897513M
Access and General Info:
- First Year Published: 1952
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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32An extended Lagrangian method
By M. S. Liou
“An extended Lagrangian method” Metadata:
- Title: An extended Lagrangian method
- Author: M. S. Liou
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1992 - 1995
- Publish Location: ➤ Springfield, Va - [Washington, D.C - [Washington, DC
“An extended Lagrangian method” Subjects and Themes:
- Subjects: ➤ Unsteady flow - Computational grids - Supersonic flow - Subsonic flow - Lagrange equations - Lagrangian function
Edition Identifiers:
- The Open Library ID: OL17124619M - OL15383946M
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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33Numerical simulation of jet aerodynamics using the three-dimensional Navier-Stokes code PAB3D
By S. Paul Pao
“Numerical simulation of jet aerodynamics using the three-dimensional Navier-Stokes code PAB3D” Metadata:
- Title: ➤ Numerical simulation of jet aerodynamics using the three-dimensional Navier-Stokes code PAB3D
- Author: S. Paul Pao
- 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
“Numerical simulation of jet aerodynamics using the three-dimensional Navier-Stokes code PAB3D” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Computational grids - Jet flow - K-epsilon turbulence model - Mach number - Navier-Stokes equation - Subsonic flow - Supersonic flow
Edition Identifiers:
- The Open Library ID: OL17838891M - OL15504438M
- Online Computer Library Center (OCLC) ID: 40386685
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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34Optical techniques for determination of normal shock position in supersonic flows for aerospace applications
By Grigory Adamovsky
“Optical techniques for determination of normal shock position in supersonic flows for aerospace applications” Metadata:
- Title: ➤ Optical techniques for determination of normal shock position in supersonic flows for aerospace applications
- Author: Grigory Adamovsky
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - NASA
- Publish Date: 1990
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Optical techniques for determination of normal shock position in supersonic flows for aerospace applications” Subjects and Themes:
- Subjects: ➤ Shock waves - Supersonic nozzles - Refractivity - Position sensing - Shock fronts - Supersonic flow - Position (Location) - Charge coupled devices - Fluid mechanics - Aerospace engineering - Fabry-Perot interferometers - Shadowgraph photography - Photodiodes
Edition Identifiers:
- The Open Library ID: OL17724916M - OL17634493M
- Online Computer Library Center (OCLC) ID: 25023003
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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35"Supersonic Gas-Liquid Cleaning System" research project
By Frank Kinney
“"Supersonic Gas-Liquid Cleaning System" research project” Metadata:
- Title: ➤ "Supersonic Gas-Liquid Cleaning System" research project
- Author: Frank Kinney
- Language: English
- Publisher: ➤ Technological Research and Development Authority, State of Florida - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - Titusville, Fla
“"Supersonic Gas-Liquid Cleaning System" research project” Subjects and Themes:
- Subjects: Cleaners - Supersonic flow - Cleaning - Supersonic nozzles - Compressed air
Edition Identifiers:
- The Open Library ID: OL15491209M - OL18116014M
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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36Doppler global velocimetry at NASA Glenn Research Center
By Christian T. Lant
“Doppler global velocimetry at NASA Glenn Research Center” Metadata:
- Title: ➤ Doppler global velocimetry at NASA Glenn Research Center
- Author: Christian T. Lant
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Technical Information Service [distributor - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2003
- Publish Location: ➤ [Cleveland, Ohio] - Springfield, VA - Hanover, MD
“Doppler global velocimetry at NASA Glenn Research Center” Subjects and Themes:
- Subjects: ➤ Coupling - Doppler effect - Free jets - Pulsed lasers - Subsonic flow - Supersonic flow - Velocity measurement
Edition Identifiers:
- The Open Library ID: OL17633151M - OL17722593M
- Online Computer Library Center (OCLC) ID: 56822084
Access and General Info:
- First Year Published: 2003
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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37Heat transfer in the transitional and turbulent boundary layers of a flat plate at supersonic speeds
By W. B. Fallis
“Heat transfer in the transitional and turbulent boundary layers of a flat plate at supersonic speeds” Metadata:
- Title: ➤ Heat transfer in the transitional and turbulent boundary layers of a flat plate at supersonic speeds
- Author: W. B. Fallis
- Number of Pages: Median: 37
- Publisher: ➤ [Institute of Aerophysics] - Institute of Aerophysics
- Publish Date: 1952
- Publish Location: ➤ [Downsview, Ont] - [Downsview, Ont.]
“Heat transfer in the transitional and turbulent boundary layers of a flat plate at supersonic speeds” Subjects and Themes:
- Subjects: Heat transfer - Supersonic flow - Turbulent boundary layer
Edition Identifiers:
- The Open Library ID: OL20897518M - OL19986943M
Access and General Info:
- First Year Published: 1952
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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38The study of supersonic flows in a shock tube
By R. Kenneth Lobb
“The study of supersonic flows in a shock tube” Metadata:
- Title: ➤ The study of supersonic flows in a shock tube
- Author: R. Kenneth Lobb
- Number of Pages: Median: 105
- Publisher: ➤ [Institute of Aerophysics] - Institute of Aerophysics
- Publish Date: 1950
- Publish Location: [Downsview, Ont.]
“The study of supersonic flows in a shock tube” Subjects and Themes:
- Subjects: Supersonic flow - Shock tubes
Edition Identifiers:
- The Open Library ID: OL21039297M - OL19986973M
Access and General Info:
- First Year Published: 1950
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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39Development of an upwind, finite-volume code with finite-rate chemistry
By Gregory A. Molvik
“Development of an upwind, finite-volume code with finite-rate chemistry” Metadata:
- Title: ➤ Development of an upwind, finite-volume code with finite-rate chemistry
- Author: Gregory A. Molvik
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - MCAT Institute - National Aeronautics and Space Administration
- Publish Date: 1994 - 1995
- Publish Location: ➤ San Jose, CA - Springfield, Va - [Washington, DC - [Washington, D.C
“Development of an upwind, finite-volume code with finite-rate chemistry” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Viscous flow - TVD schemes - Three dimensional bodies - Reacting flow - Upwind schemes (Mathematics) - Engine airframe integration - Hypersonic flow - Supersonic flow - Finite volume method - Finite difference theory - Gases - Algorithms - Computer programs - Hypersonic vehicles
Edition Identifiers:
- The Open Library ID: OL15413734M - OL15381561M
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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40Porous and microporous honeycomb composites as potential boundary-layer bleed materials
By D. O. Davis
“Porous and microporous honeycomb composites as potential boundary-layer bleed materials” Metadata:
- Title: ➤ Porous and microporous honeycomb composites as potential boundary-layer bleed materials
- Author: D. O. Davis
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“Porous and microporous honeycomb composites as potential boundary-layer bleed materials” Subjects and Themes:
- Subjects: ➤ Boundary layer control - Honeycomb structures - Composite materials - Supersonic flow - Wind tunnel tests - Mach number
Edition Identifiers:
- The Open Library ID: OL15539875M - OL17838310M
- Online Computer Library Center (OCLC) ID: 40758884
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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41Investigation of ramp injectors for supersonic mixing enhancement
By Y. Haimovitch
“Investigation of ramp injectors for supersonic mixing enhancement” Metadata:
- Title: ➤ Investigation of ramp injectors for supersonic mixing enhancement
- Author: Y. Haimovitch
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1994
- Publish Location: [Springfield, VA - Hampton, Va
“Investigation of ramp injectors for supersonic mixing enhancement” Subjects and Themes:
- Subjects: ➤ Nozzle inserts - Fuel injection - Supersonic flow - Nozzle geometry - Supersonic combustion ramjet engines - Turbulent mixing - Spray nozzles - Wind tunnel tests - Injectors
Edition Identifiers:
- The Open Library ID: OL15409145M - OL17790638M
- Online Computer Library Center (OCLC) ID: 32712612
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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42Supersonic flow computations for an ASTOVL aircraft configuration
By Sekaripuram Ramakrishnan
“Supersonic flow computations for an ASTOVL aircraft configuration” Metadata:
- Title: ➤ Supersonic flow computations for an ASTOVL aircraft configuration
- Author: Sekaripuram Ramakrishnan
- Language: English
- Number of Pages: Median: 40
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - Langley Research Center
- Publish Date: 1990
- Publish Location: ➤ [Washington, D.C.] - Hampton, Va
“Supersonic flow computations for an ASTOVL aircraft configuration” Subjects and Themes:
- Subjects: ➤ Supersonic flow - Computational fluid dynamics - Short takeoff aircraft - Grid generation (Mathematics) - Aircraft configurations - V/STOL aircraft - Design analysis
Edition Identifiers:
- The Open Library ID: OL16135381M - OL20268695M
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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Downloads Are Not Available:
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43Investigation of mixing a supersonic stream with the flow downstream of a wedge
By Joseph Sheeley
“Investigation of mixing a supersonic stream with the flow downstream of a wedge” Metadata:
- Title: ➤ Investigation of mixing a supersonic stream with the flow downstream of a wedge
- Author: Joseph Sheeley
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Investigation of mixing a supersonic stream with the flow downstream of a wedge” Subjects and Themes:
- Subjects: ➤ Velocity distribution - Supersonic flow - Flow distribution - Air flow - Flow visualization - Mach number - Gas injection - Multiphase flow - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15538185M - OL17837879M
- Online Computer Library Center (OCLC) ID: 40563313
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:
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44The simulation of three-dimensional viscous supersonic flow past blunt bodies with a hybrid implicit/explicit finite-difference method
By Stefan Riedelbauch
“The simulation of three-dimensional viscous supersonic flow past blunt bodies with a hybrid implicit/explicit finite-difference method” Metadata:
- Title: ➤ The simulation of three-dimensional viscous supersonic flow past blunt bodies with a hybrid implicit/explicit finite-difference method
- Author: Stefan Riedelbauch
- Language: English
- Number of Pages: Median: 58
- Publisher: DFVLR
- Publish Date: 1987
- Publish Location: Köln - Koln
“The simulation of three-dimensional viscous supersonic flow past blunt bodies with a hybrid implicit/explicit finite-difference method” Subjects and Themes:
- Subjects: Navier-Stokes equation - Heat flux - Blunt bodies - Supersonic flow - Finite difference theory
Edition Identifiers:
- The Open Library ID: OL47989003M - OL19249642M
- Online Computer Library Center (OCLC) ID: 22330780
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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45An exact theory of supersonic flow around a delta wing
By L. R. Fowell
“An exact theory of supersonic flow around a delta wing” Metadata:
- Title: ➤ An exact theory of supersonic flow around a delta wing
- Author: L. R. Fowell
- Number of Pages: Median: 92
- Publisher: ➤ [Institute of Aerophysics] - Institute of Aerophysics
- Publish Date: 1955
- Publish Location: [Downsview, Ont.]
“An exact theory of supersonic flow around a delta wing” Subjects and Themes:
- Subjects: Conical flow - Supersonic flow - Delta wings
Edition Identifiers:
- The Open Library ID: OL20985528M - OL20897560M
Access and General Info:
- First Year Published: 1955
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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46Effects of probe size on measurements in a laminar boundary layer in supersonic flow
By G. R. Ludwig
“Effects of probe size on measurements in a laminar boundary layer in supersonic flow” Metadata:
- Title: ➤ Effects of probe size on measurements in a laminar boundary layer in supersonic flow
- Author: G. R. Ludwig
- Publisher: ➤ Institute of Aerophysics - Dept. of Aeronautical Engineering and Aerophysics
- Publish Date: 1956
- Publish Location: [Downsview, Ont.]
“Effects of probe size on measurements in a laminar boundary layer in supersonic flow” Subjects and Themes:
- Subjects: Laminar boundary layer - Supersonic flow - Probes
Edition Identifiers:
- The Open Library ID: OL18999708M - OL19003962M
Access and General Info:
- First Year Published: 1956
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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47Laser beam propagation through inhomogeneous media with shock-like profiles
By Grigory Adamovsky
“Laser beam propagation through inhomogeneous media with shock-like profiles” Metadata:
- Title: ➤ Laser beam propagation through inhomogeneous media with shock-like profiles
- Author: Grigory Adamovsky
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Cleveland, Ohio] - [Springfield, Va
“Laser beam propagation through inhomogeneous media with shock-like profiles” Subjects and Themes:
- Subjects: ➤ Flow visualization - Laser beams - Radio transmission - Radio waves - Supersonic flow - Thin films - Wave guides - Wave propagation - Waveguides
Edition Identifiers:
- The Open Library ID: OL15539865M - OL17838309M
- Online Computer Library Center (OCLC) ID: 40747075
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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Downloads Are Not Available:
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48An asymptotic analysis of supersonic reacting mixing layers
By Thomas L. Jackson
“An asymptotic analysis of supersonic reacting mixing layers” Metadata:
- Title: ➤ An asymptotic analysis of supersonic reacting mixing layers
- Author: Thomas L. Jackson
- Number of Pages: Median: 14
- Publisher: ICASE
- Publish Date: 1987
- Publish Location: Hampton, Va
“An asymptotic analysis of supersonic reacting mixing layers” Subjects and Themes:
- Subjects: Asymptotic methods - Supersonic flow
Edition Identifiers:
- The Open Library ID: OL19000166M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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49Aerodynamic shape optimization directed toward a supersonic transport using sensitivity analysis
By Oktay Baysal
“Aerodynamic shape optimization directed toward a supersonic transport using sensitivity analysis” Metadata:
- Title: ➤ Aerodynamic shape optimization directed toward a supersonic transport using sensitivity analysis
- Author: Oktay Baysal
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Dept. of Aerospace Engineering, College of Engineering & Technology, Old Dominion University - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, D.C - Norfolk, Va
“Aerodynamic shape optimization directed toward a supersonic transport using sensitivity analysis” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Aircraft design - Algorithms - Computational fluid dynamics - Computer aided design - Design analysis - Optimization - Shapes - Supersonic flow - Viscous flow
Edition Identifiers:
- The Open Library ID: OL15419489M
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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50Shear flow control of cold and heated rectangular jets by mechanical tabs
By W. H. Brown
“Shear flow control of cold and heated rectangular jets by mechanical tabs” Metadata:
- Title: ➤ Shear flow control of cold and heated rectangular jets by mechanical tabs
- Author: W. H. Brown
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1989
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Shear flow control of cold and heated rectangular jets by mechanical tabs” Subjects and Themes:
- Subjects: ➤ Boundary layer flow - Flow measurement - Free jets - Jet flow - Jet mixing flow - Nozzle design - Nozzle flow - Nozzle inserts - Shear flow - Subsonic flow - Supersonic flow - Tabs (Control surfaces)
Edition Identifiers:
- The Open Library ID: OL17002529M
Access and General Info:
- First Year Published: 1989
- 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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