Explore: Boundary Layer Transition
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Source: The Open Library
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1Large-eddy simulation of laminar-turbulent breakdown at high speeds with dynamic subgrid-scale modeling
By Nabil M. El-Hady
“Large-eddy simulation of laminar-turbulent breakdown at high speeds with dynamic subgrid-scale modeling” Metadata:
- Title: ➤ Large-eddy simulation of laminar-turbulent breakdown at high speeds with dynamic subgrid-scale modeling
- Author: Nabil M. El-Hady
- Language: English
- Number of Pages: Median: 57
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - Langley Research Center - National Technical Information Service, distributor]
- Publish Date: 1993
- Publish Location: ➤ [Washington, DC] - Hampton, Va - [Washington, D.C.] - [Springfield, Va
“Large-eddy simulation of laminar-turbulent breakdown at high speeds with dynamic subgrid-scale modeling” Subjects and Themes:
- Subjects: ➤ Boundary layer - Fluid mechanics - Boundary layer flow - Computational fluid dynamics - Large eddy simulation - Compressible boundary layer - Flow distribution - Boundary layer transition - Transition flow
Edition Identifiers:
- The Open Library ID: ➤ OL17751653M - OL19916688M - OL15387886M - OL17111221M - OL18065538M - OL15418767M - OL18084323M
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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2Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements
By W. Lance Richards
“Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements” Metadata:
- Title: ➤ Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements
- Author: W. Lance Richards
- Language: English
- Number of Pages: Median: 14
- Publisher: ➤ Available from the NASA Center for AeroSpace Information] - National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - [Linthicum Heights, MD - [Washington, D.C.]
“Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Aerodynamics, Hypersonic - Boundary layer transition - Data processing - Design and construction - Finite element method - Hypersonic Aerodynamics - Hypersonic planes - Hypersonic speed - Leading edges - Research - Structural design
Edition Identifiers:
- The Open Library ID: OL18134772M - OL19433479M - OL15548269M - OL17132909M - OL17839410M
- Online Computer Library Center (OCLC) ID: 41975259
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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3Assessment of dual-point drag reduction for an executive-jet modified airfoil section
By Dennis O. Allison
“Assessment of dual-point drag reduction for an executive-jet modified airfoil section” Metadata:
- Title: ➤ Assessment of dual-point drag reduction for an executive-jet modified airfoil section
- Author: Dennis O. Allison
- Language: English
- Number of Pages: Median: 114
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - Available from National Technical Information Center - National Technical Information Service, distributor - National Aeronautics and Space Administration, Langly Research Center
- Publish Date: 1996
- Publish Location: ➤ Hampton, Virginia - Springfield, VA - Hampton, Va - [Springfield, Va
“Assessment of dual-point drag reduction for an executive-jet modified airfoil section” Subjects and Themes:
- Subjects: ➤ Drag reduction - Reynolds number - Boundary layer transition - Angle of attack - Pitching moments - Transonic wind tunnels - Airfoil profiles - Force distribution - Trailing edges - Aerodynamic characteristics - Aerodynamics - Aerofoils
Edition Identifiers:
- The Open Library ID: OL19049550M - OL18121248M - OL17126940M - OL17581020M - OL15504416M
- Online Computer Library Center (OCLC) ID: 40386607
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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4Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate)
By M. N. Kogan
“Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate)” Metadata:
- Title: ➤ Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate)
- Author: M. N. Kogan
- Language: English
- Number of Pages: Median: 44
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center - Available from NASA Center for AeroSpace Information
- Publish Date: 1997
- Publish Location: ➤ Linthicum Heights, MD - [Springfield, Va - Hampton, Va
“Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate)” Subjects and Themes:
- Subjects: ➤ Amplification - Boundary layer - Boundary layer flow - Boundary layer transition - Boundary layers - Flow distortion - Free flow - Inhomogeneity - Laminar flow - Leading edges - Nonuniformity - Reynolds number - Vortex-motion - Wakes - Wire
Edition Identifiers:
- The Open Library ID: OL20887494M - OL18122412M - OL15508905M - OL17574799M - OL17126862M
- Online Computer Library Center (OCLC) ID: 40341327
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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5Development 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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6Swept-wing receptivity studies using distributed roughness
By W. S. Saric
“Swept-wing receptivity studies using distributed roughness” Metadata:
- Title: ➤ Swept-wing receptivity studies using distributed roughness
- Author: W. S. Saric
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Mechanical and Aerospace Engineering, College of Engineering and Applied Science, Arizona State University - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1998
- Publish Location: ➤ Hampton, Va - [Springfield, Va - Tempe, AZ
“Swept-wing receptivity studies using distributed roughness” Subjects and Themes:
- Subjects: Pressure gradients - Cross flow - Swept wings - Nonlinearity - Boundary layer transition
Edition Identifiers:
- The Open Library ID: OL17583482M - OL15547477M - OL17132992M - OL18134575M
- Online Computer Library Center (OCLC) ID: 41993468
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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7Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment
By Laurie A. Marshall
“Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment” Metadata:
- Title: ➤ Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment
- Author: Laurie A. Marshall
- Language: English
- Number of Pages: Median: 48
- Publisher: ➤ NASA Center for AeroSpace Information [distributor] - National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service [distributor - Available from NASA Center for AeroSpace Information
- Publish Date: 1999
- Publish Location: ➤ Springfield, VA - Edwards, Calif - Hanover, Md - Hanover, MD
“Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment” Subjects and Themes:
- Subjects: ➤ Boundary layer - Boundary layer control - Boundary layer transition - F-16 (Jet fighter plane) - Laminar boundary layer - Laminar flow - Supersonic Aerodynamics
Edition Identifiers:
- The Open Library ID: OL15563026M - OL20639543M - OL17593816M - OL18139199M
- Online Computer Library Center (OCLC) ID: 43704178
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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8Validation of three-dimensional incompressible spatial direct numerical simulation code
By Ronald D. Joslin
“Validation of three-dimensional incompressible spatial direct numerical simulation code” Metadata:
- Title: ➤ Validation of three-dimensional incompressible spatial direct numerical simulation code
- Author: Ronald D. Joslin
- Language: English
- Number of Pages: Median: 46
- Publisher: ➤ Langley Research Center - For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1992
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, DC]
“Validation of three-dimensional incompressible spatial direct numerical simulation code” Subjects and Themes:
- Subjects: ➤ Computer simulation - Stability - Boundary layer - Transition flow - Boundary layer transition - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL19245005M - OL15366306M - OL14684889M - OL18055438M
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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9Flow-separation patterns on symmetric forebodies
By Earl R. Keener
“Flow-separation patterns on symmetric forebodies” Metadata:
- Title: ➤ Flow-separation patterns on symmetric forebodies
- Author: Earl R. Keener
- Language: English
- Number of Pages: Median: 135
- Publisher: ➤ For sale by the National Technical Information Service] - Ames Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1986 - 1987
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif - [Washington, DC]
“Flow-separation patterns on symmetric forebodies” Subjects and Themes:
- Subjects: ➤ Flow visualization - Vortex shedding - Boundary layer transition - Reynolds number - Aerodynamics - Mach number - Angle of attack
Edition Identifiers:
- The Open Library ID: OL18032518M - OL17099358M - OL19985950M - OL15288167M
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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10Distributed-roughness effects on stability and transition in swept-wing boundary layers
By Ruben B. Carrillo
“Distributed-roughness effects on stability and transition in swept-wing boundary layers” Metadata:
- Title: ➤ Distributed-roughness effects on stability and transition in swept-wing boundary layers
- Author: Ruben B. Carrillo
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Distributed-roughness effects on stability and transition in swept-wing boundary layers” Subjects and Themes:
- Subjects: ➤ Airfoils - Boundary layer stability - Boundary layer transition - Cross flow - Flow visualization - Surface roughness - Swept wings - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17128387M - OL17597200M - OL18132177M - OL15540242M
- Online Computer Library Center (OCLC) ID: 40717111
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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11Supersonic quiet-tunnel development for laminar-turbulent transition research
By Steven P. Schneider
“Supersonic quiet-tunnel development for laminar-turbulent transition research” Metadata:
- Title: ➤ Supersonic quiet-tunnel development for laminar-turbulent transition research
- Author: Steven P. Schneider
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Supersonic quiet-tunnel development for laminar-turbulent transition research” Subjects and Themes:
- Subjects: ➤ Boundary layer equations - Boundary layer transition - Flow characteristics - Flow measurement - Nozzle walls - Supersonic wind tunnels - Wall flow - Wind tunnel nozzles - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL18082383M - OL15415636M - OL17791329M
- Online Computer Library Center (OCLC) ID: 33200505
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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12Non-linear boundary-layer receptivity due to distributed surface roughness
By Gregory V. Selby
“Non-linear boundary-layer receptivity due to distributed surface roughness” Metadata:
- Title: ➤ Non-linear boundary-layer receptivity due to distributed surface roughness
- Author: Gregory V. Selby
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - Old Dominion University Research Foundation, Dept. of Mechanical Engineering, College of Engineering & Technology - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C - Norfolk, Va - Springfield, Va
“Non-linear boundary-layer receptivity due to distributed surface roughness” Subjects and Themes:
- Subjects: ➤ Boundary layer flow - Boundary layer stability - Boundary layer transition - Laminar boundary layer - Surface roughness - Surface roughness effects - Tollmien-Schlichting waves - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL18084770M - OL15419714M - OL17793565M
- Online Computer Library Center (OCLC) ID: 34736159
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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13Supersonic 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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14Two-equation low-Reynolds-number turbulence modeling of transitional boundary layer flows characteristic of gas turbine blades
By Rodney C. Schmidt
“Two-equation low-Reynolds-number turbulence modeling of transitional boundary layer flows characteristic of gas turbine blades” Metadata:
- Title: ➤ Two-equation low-Reynolds-number turbulence modeling of transitional boundary layer flows characteristic of gas turbine blades
- Author: Rodney C. Schmidt
- Language: English
- Number of Pages: Median: 261
- Publisher: ➤ For sale by the National Technical Information Service] - Lewis Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Division
- Publish Date: 1988
- Publish Location: ➤ Cleveland, Ohio - [Washington, DC] - [Springfield, Va
“Two-equation low-Reynolds-number turbulence modeling of transitional boundary layer flows characteristic of gas turbine blades” Subjects and Themes:
- Subjects: ➤ Transmission - Transition flow - Turbulence models - Turbines - Heat - Boundary layer transition - Turbine blades - Blades
Edition Identifiers:
- The Open Library ID: OL15377550M - OL18060436M - OL20898705M
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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15A k-E [i.e. Kappa-Epsilon] calculation of transitional boundary layers
By Z. Yang
“A k-E [i.e. Kappa-Epsilon] calculation of transitional boundary layers” Metadata:
- Title: ➤ A k-E [i.e. Kappa-Epsilon] calculation of transitional boundary layers
- Author: Z. Yang
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - NASA
- Publish Date: 1992
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“A k-E [i.e. Kappa-Epsilon] calculation of transitional boundary layers” Subjects and Themes:
- Subjects: ➤ Boundary layer transition - Boundary layers - Boundary value problems - K-epsilon turbulence model - Low Reynolds number - Transition flow - Turbulent flow
Edition Identifiers:
- The Open Library ID: OL15500317M - OL18119606M - OL17125005M
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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16Boundary-layer receptivity due to distributed surface imperfections of a deterministic or random nature
By Meelan Choudhari
“Boundary-layer receptivity due to distributed surface imperfections of a deterministic or random nature” Metadata:
- Title: ➤ Boundary-layer receptivity due to distributed surface imperfections of a deterministic or random nature
- Author: Meelan Choudhari
- Language: English
- Number of Pages: Median: 18
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - Langley Research Center
- Publish Date: 1992
- Publish Location: ➤ [Washington, D.C.] - Hampton, Va
“Boundary-layer receptivity due to distributed surface imperfections of a deterministic or random nature” Subjects and Themes:
- Subjects: ➤ Transtion flow - Boundary layers - Sound waves - Surface roughness - Boundary layer flow - Random processes - Flow stability - Boundary layer transition - Receptivity - Surface defects
Edition Identifiers:
- The Open Library ID: OL19244514M - OL18226192M - OL16123781M
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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17Boundary-layer transition and global skin friction measurement with an oil-fringe imaging technique
By Daryl J. Monson
“Boundary-layer transition and global skin friction measurement with an oil-fringe imaging technique” Metadata:
- Title: ➤ Boundary-layer transition and global skin friction measurement with an oil-fringe imaging technique
- Author: Daryl J. Monson
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1993
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Boundary-layer transition and global skin friction measurement with an oil-fringe imaging technique” Subjects and Themes:
- Subjects: ➤ Skin friction - Wind tunnel tests - Oils - Imaging techniques - Boundary layer transition - Wind tunnel models - Friction measurement - Wings
Edition Identifiers:
- The Open Library ID: OL18081875M - OL15414994M - OL17792152M
- Online Computer Library Center (OCLC) ID: 33973439
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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18Flight-measured laminar boundary-layer transition phenomena including stability theory analysis
By Clifford J. Obara
“Flight-measured laminar boundary-layer transition phenomena including stability theory analysis” Metadata:
- Title: ➤ Flight-measured laminar boundary-layer transition phenomena including stability theory analysis
- Author: Clifford J. Obara
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service,] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1985
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Flight-measured laminar boundary-layer transition phenomena including stability theory analysis” Subjects and Themes:
- Subjects: ➤ Laminar flow - Turbulent boundary layer - Aerodynamic coefficients - Boundary layer transition - Boundary layer - Transition flow
Edition Identifiers:
- The Open Library ID: OL16115008M - OL18217710M - OL18468555M
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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19The velocity field created by a shallow bump in a boundary layer
By Michael Gaster
“The velocity field created by a shallow bump in a boundary layer” Metadata:
- Title: ➤ The velocity field created by a shallow bump in a boundary layer
- Author: Michael Gaster
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Institute for Computer Applications in Science and Engineering, NASA Langley Research Center
- Publish Date: 1994
- Publish Location: [Springfield, Va - Hampton, VA
“The velocity field created by a shallow bump in a boundary layer” Subjects and Themes:
- Subjects: ➤ Boundary layer flow - Boundary layer transition - Boundary layers - Flat plates - Oscillating flow - Small perturbation flow - Velocity distribution - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17791798M - OL15418859M
- Online Computer Library Center (OCLC) ID: 34067477
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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20Instantaneous structure of turbulent separated boundary layers
By R. J. Adrian
“Instantaneous structure of turbulent separated boundary layers” Metadata:
- Title: ➤ Instantaneous structure of turbulent separated boundary layers
- Author: R. J. Adrian
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Instantaneous structure of turbulent separated boundary layers” Subjects and Themes:
- Subjects: Boundary layer transition - Fluid mechanics - Thermal boundary layer - Turbulent boundary layer
Edition Identifiers:
- The Open Library ID: OL17837677M - OL15509250M
- Online Computer Library Center (OCLC) ID: 40483480
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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21The structure of separated flow regions occurring near the leading edge of airfoils, including transition
By T. J. Mueller
“The structure of separated flow regions occurring near the leading edge of airfoils, including transition” Metadata:
- Title: ➤ The structure of separated flow regions occurring near the leading edge of airfoils, including transition
- Author: T. J. Mueller
- Language: English
- Publisher: ➤ National Technical Information Service - National Technical Information Service, distributor - Dept. of Aerospace and Mechanical Engineering, University of Notre Dame - National Aeronautics and Space Administration
- Publish Date: 1985 - 1986
- Publish Location: ➤ Notre Dame, Ind - [Springfield, Va - [Washington, D.C - Springfield, Va
“The structure of separated flow regions occurring near the leading edge of airfoils, including transition” Subjects and Themes:
- Subjects: ➤ Aerofoils - Airfoils - Boundary layer transition - Bubbles - Leading edges - Separated flow - Velocity distribution
Edition Identifiers:
- The Open Library ID: OL15416442M - OL15394429M
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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22Special course on progress in transition modelling
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
“Special course on progress in transition modelling” Metadata:
- Title: ➤ Special course on progress in transition modelling
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
- Language: English
- Number of Pages: Median: 276
- Publisher: AGARD - Agard
- Publish Date: 1994
- Publish Location: ➤ Neuilly sur Seine - Neuilly-sur-Seine, France
“Special course on progress in transition modelling” Subjects and Themes:
- Subjects: Boundary layer transition - Transition flow - Transition modelling
Edition Identifiers:
- The Open Library ID: OL19687002M - OL19754533M
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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23Computation of three-dimensional boundary layers including separation
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
“Computation of three-dimensional boundary layers including separation” Metadata:
- Title: ➤ Computation of three-dimensional boundary layers including separation
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
- Language: English
- Publisher: Sine nomine - AGARD
- Publish Date: 1987
- Publish Location: ➤ S.l - Neuilly sur Seine, France
“Computation of three-dimensional boundary layers including separation” Subjects and Themes:
- Subjects: Aerodynamic characteristics - Boundary layer flow - Boundary layer separation - Boundary layer transition - Turbulent flow
Edition Identifiers:
- The Open Library ID: OL21697122M - OL18999282M
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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24Instability and transition of flow at, and near, an attachment-line
By A. Smith
“Instability and transition of flow at, and near, an attachment-line” Metadata:
- Title: ➤ Instability and transition of flow at, and near, an attachment-line
- Author: A. Smith
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996 - 1998
- Publish Location: ➤ Hampton, Va - [Washington, DC - [Springfield, Va - Springfield, Va
“Instability and transition of flow at, and near, an attachment-line” Subjects and Themes:
- Subjects: ➤ Boundary layer control - Boundary layer transition - Boundary layers - Control surfaces - Drag - Laminar boundary layer - Reynolds number - Stability - Transition flow - Turbulence - Wings
Edition Identifiers:
- The Open Library ID: OL15544664M - OL15547327M
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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25Thermal analysis of a metallic wing glove for a Mach-8 boundary-layer experiment
By Leslie Gong
“Thermal analysis of a metallic wing glove for a Mach-8 boundary-layer experiment” Metadata:
- Title: ➤ Thermal analysis of a metallic wing glove for a Mach-8 boundary-layer experiment
- Author: Leslie Gong
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Dryden Flight Research Center
- Publish Date: 1998
- Publish Location: ➤ Springfield, VA - Edwards, Calif
“Thermal analysis of a metallic wing glove for a Mach-8 boundary-layer experiment” Subjects and Themes:
- Subjects: ➤ Hypersonic speed - Finite element method - Aerodynamic heating - Thermal analysis - Boundary layer transition - Design analysis
Edition Identifiers:
- The Open Library ID: OL15541774M - OL17838703M
- Online Computer Library Center (OCLC) ID: 41214761
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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26Some problems in boundary-layer transition
By J. A. Steketee
“Some problems in boundary-layer transition” Metadata:
- Title: ➤ Some problems in boundary-layer transition
- Author: J. A. Steketee
- Language: English
- Number of Pages: Median: 95
- Publisher: ➤ Sine nomine - Institute of Aerophysics
- Publish Date: 1954 - 1956
- Publish Location: [Downsview, Ont.] - Toronto
“Some problems in boundary-layer transition” Subjects and Themes:
- Subjects: Boundary layer transition
Edition Identifiers:
- The Open Library ID: OL14852770M - OL20897580M
Access and General Info:
- First Year Published: 1954
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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27Hybrid laminar flow control experiments in the NASA - Ames, 11-foot tunnel
By W. S. Saric
“Hybrid laminar flow control experiments in the NASA - Ames, 11-foot tunnel” Metadata:
- Title: ➤ Hybrid laminar flow control experiments in the NASA - Ames, 11-foot tunnel
- Author: W. S. Saric
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“Hybrid laminar flow control experiments in the NASA - Ames, 11-foot tunnel” Subjects and Themes:
- Subjects: ➤ Drag reduction - Surface roughness effects - Wind tunnel tests - Swept wings - Laminar boundary layer - Boundary layer control - Boundary layer transition - Turbulence effects
Edition Identifiers:
- The Open Library ID: OL15423184M - OL17796516M
- Online Computer Library Center (OCLC) ID: 35290580
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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28Non-linear evolution of a second mode wave in supersonic boundary layers
By Gordon Erlebacher
“Non-linear evolution of a second mode wave in supersonic boundary layers” Metadata:
- Title: ➤ Non-linear evolution of a second mode wave in supersonic boundary layers
- Author: Gordon Erlebacher
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Institute for Computer Applications in Science and Engineering, NASA Langley Research Center
- Publish Date: 1989
- Publish Location: [Springfield, Va - Hampton, VA
“Non-linear evolution of a second mode wave in supersonic boundary layers” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Boundary value problems - Computerized simulation - Supersonic boundary layers - Channel flow - Flow stability - Wall flow - Boundary layer transition - Wave generation - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL15407774M - OL18078350M
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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29Solar rocket plume/mirror interactions
By Sheng-Tao Yu
“Solar rocket plume/mirror interactions” Metadata:
- Title: ➤ Solar rocket plume/mirror interactions
- Author: Sheng-Tao Yu
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration
- Publish Date: 1991
- Publish Location: [Washington, D.C.]
“Solar rocket plume/mirror interactions” Subjects and Themes:
- Subjects: ➤ Boundary layer transition - Continuums - Fouling - Hydrogen fuels - Navier-Stokes equation - Pressure distribution - Pressure effects - Solar thermal propulsion - Viscous flow
Edition Identifiers:
- The Open Library ID: OL17632392M - OL16133038M
- Online Computer Library Center (OCLC) ID: 63906446
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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30Multiple paths to subharmonic laminar breakdown in a boundary layer
By Thomas A. Zang
“Multiple paths to subharmonic laminar breakdown in a boundary layer” Metadata:
- Title: ➤ Multiple paths to subharmonic laminar breakdown in a boundary layer
- Author: Thomas A. Zang
- Language: English
- Number of Pages: Median: 12
- Publisher: ➤ Institute for Computer Applications in Science and Engineering - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1989 - 1990
- Publish Location: Hampton, Va
“Multiple paths to subharmonic laminar breakdown in a boundary layer” Subjects and Themes:
- Subjects: Transmission - Heat - Fluid mechanics - Boundary layer transition
Edition Identifiers:
- The Open Library ID: OL19380306M - OL15276194M
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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31Experimental study of boundary layer behavior in a simulated low pressure turbine
By Rickey J. Shyne
“Experimental study of boundary layer behavior in a simulated low pressure turbine” Metadata:
- Title: ➤ Experimental study of boundary layer behavior in a simulated low pressure turbine
- Author: Rickey J. Shyne
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ [Cleveland, Ohio] - [Springfield, Va
“Experimental study of boundary layer behavior in a simulated low pressure turbine” Subjects and Themes:
- Subjects: ➤ Turbulent flow - Turbulent boundary layer - Fluid dynamics - Boundary layer separation - Wind tunnel tests - Turbines - Low pressure - Flow visualization - Boundary layer transition - Flow measurement
Edition Identifiers:
- The Open Library ID: OL17839326M - OL15546581M
- Online Computer Library Center (OCLC) ID: 41553970
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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32Wall shear stress measurements on a prolate spheroid at zero incidence in the DNW wind tunnel
By Hans-Peter Kreplin
“Wall shear stress measurements on a prolate spheroid at zero incidence in the DNW wind tunnel” Metadata:
- Title: ➤ Wall shear stress measurements on a prolate spheroid at zero incidence in the DNW wind tunnel
- Author: Hans-Peter Kreplin
- Language: English
- Number of Pages: Median: 38
- Publisher: DFVLR - Koln
- Publish Date: 1986
- Publish Location: Köln - Gottingen
“Wall shear stress measurements on a prolate spheroid at zero incidence in the DNW wind tunnel” Subjects and Themes:
- Subjects: Prolate spheroids - Boundary layer transition
Edition Identifiers:
- The Open Library ID: OL47989108M - OL19986559M
- Online Computer Library Center (OCLC) ID: 27269194
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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33Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction
By D. O. Davis
“Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction” Metadata:
- Title: ➤ Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction
- Author: D. O. Davis
- 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
“Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction” Subjects and Themes:
- Subjects: ➤ Turbulent boundary layer - Flow measurement - Mass flow - Oblique shock waves - Boundary layer control - Boundary layer transition - Interactional aerodynamics - Slots - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15541815M - OL17838705M
- Online Computer Library Center (OCLC) ID: 41323463
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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34Acoustic excitation of Tollmien-Schlichting waves in a laminar boundary layer
By Norman George Ball
“Acoustic excitation of Tollmien-Schlichting waves in a laminar boundary layer” Metadata:
- Title: ➤ Acoustic excitation of Tollmien-Schlichting waves in a laminar boundary layer
- Author: Norman George Ball
- Publisher: ➤ [Institute for Aerospace Studies] - Institute for Aerospace Studies
- Publish Date: 1987
- Publish Location: [Downsview, Ont.]
“Acoustic excitation of Tollmien-Schlichting waves in a laminar boundary layer” Subjects and Themes:
- Subjects: ➤ Tollmien-Schlichting waves - Boundary layer transition - Boundary layer stability - Acoustic excitation - Plane waves - Laminar boundary layer
Edition Identifiers:
- The Open Library ID: OL20986791M - OL18999352M
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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35Statistical prediction of laminar-turbulent transition
By Robert Rubinstein
“Statistical prediction of laminar-turbulent transition” Metadata:
- Title: ➤ Statistical prediction of laminar-turbulent transition
- Author: Robert Rubinstein
- Language: English
- Publisher: ➤ Institute for Computer Applications in Science and Engineering, NASA Langley Research Center - National Technical Information Service, distributor
- Publish Date: 2000
- Publish Location: Springfield, VA - Hampton, VA
“Statistical prediction of laminar-turbulent transition” Subjects and Themes:
- Subjects: ➤ Boundary layer transition - Laminar flow - Mathematical models - Prediction analysis techniques - Statistical analysis - Stochastic processes - Transition flow - Turbulence models - Turbulent flow
Edition Identifiers:
- The Open Library ID: OL17601385M - OL16012132M
Access and General Info:
- First Year Published: 2000
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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36Stability in aerospace systems
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
“Stability in aerospace systems” Metadata:
- Title: Stability in aerospace systems
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
- Number of Pages: Median: 234
- Publisher: AGARD
- Publish Date: 1993
- Publish Location: Neuilly-sur-Seine, France
“Stability in aerospace systems” Subjects and Themes:
- Subjects: Boundary layer transition - Stability
Edition Identifiers:
- The Open Library ID: OL19917496M
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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37Hypersonic boundary-layer transition for X-33 phase II vehicle
By R. A. Thompson
“Hypersonic boundary-layer transition for X-33 phase II vehicle” Metadata:
- Title: ➤ Hypersonic boundary-layer transition for X-33 phase II vehicle
- Author: R. A. Thompson
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - American Institute of Aeronautics and Astronautics - National Aeronautics and Space Administration
- Publish Date: 1998
- Publish Location: ➤ Reston, Va - [Washington, DC - Springfield, Va
“Hypersonic boundary-layer transition for X-33 phase II vehicle” Subjects and Themes:
- Subjects: ➤ Flow visualization - Boundary layer transition - Hypersonics - Finite volume method - Wind tunnel tests - Flow distribution
Edition Identifiers:
- The Open Library ID: OL17578604M
- Online Computer Library Center (OCLC) ID: 40771865
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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38Numerical modeling studies of wake vortex transport and evolution within the planetary boundary layer
By Yuh-Lang Lin
“Numerical modeling studies of wake vortex transport and evolution within the planetary boundary layer” Metadata:
- Title: ➤ Numerical modeling studies of wake vortex transport and evolution within the planetary boundary layer
- Author: Yuh-Lang Lin
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1998
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Numerical modeling studies of wake vortex transport and evolution within the planetary boundary layer” Subjects and Themes:
- Subjects: ➤ Large eddy simulation - Atmospheric turbulence - Wakes - Atmospheric boundary layer - Vortices - Kinetic energy - Boundary layer transition
Edition Identifiers:
- The Open Library ID: OL17839171M
- Online Computer Library Center (OCLC) ID: 41679273
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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39Some characteristics of bypass transition in a heated boundary layer
By Ki-Hyeon Sohn
“Some characteristics of bypass transition in a heated boundary layer” Metadata:
- Title: ➤ Some characteristics of bypass transition in a heated boundary layer
- Author: Ki-Hyeon Sohn
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1989
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Some characteristics of bypass transition in a heated boundary layer” Subjects and Themes:
- Subjects: ➤ Laminar boundary layer - Heat transfer - Flat plates - Boundary layer transition - Turbulent boundary layer - Bypass ratio
Edition Identifiers:
- The Open Library ID: OL15408225M
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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40Numerical simulation of nonlinear receptivity in boundary layer transition
By Hermann F. Fasel
“Numerical simulation of nonlinear receptivity in boundary layer transition” Metadata:
- Title: ➤ Numerical simulation of nonlinear receptivity in boundary layer transition
- Author: Hermann F. Fasel
- Publisher: ➤ University of Arizona, Engineering Experiment Station
- Publish Date: 1990
- Publish Location: Tucson, Ariz
“Numerical simulation of nonlinear receptivity in boundary layer transition” Subjects and Themes:
- Subjects: Boundary layer transition
Edition Identifiers:
- The Open Library ID: OL21499380M
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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41Some characteristics of bypass transition in a heated boundary layer
By K. H. Sohn
“Some characteristics of bypass transition in a heated boundary layer” Metadata:
- Title: ➤ Some characteristics of bypass transition in a heated boundary layer
- Author: K. H. Sohn
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1989
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Some characteristics of bypass transition in a heated boundary layer” Subjects and Themes:
- Subjects: ➤ Laminar boundary layer - Heat transfer - Flat plates - Boundary layer transition - Turbulent boundary layer - Bypass ratio
Edition Identifiers:
- The Open Library ID: OL17114594M
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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42Advanced boundary layer transition measurement methods for flight applications
By Bruce J. Holmes
“Advanced boundary layer transition measurement methods for flight applications” Metadata:
- Title: ➤ Advanced boundary layer transition measurement methods for flight applications
- Author: Bruce J. Holmes
- Number of Pages: Median: 13
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1986
- Publish Location: New York
“Advanced boundary layer transition measurement methods for flight applications” Subjects and Themes:
- Subjects: Boundary layer transition
Edition Identifiers:
- The Open Library ID: OL21333398M
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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43Analytical and experimental verification of a flight article for a Mach-8 boundary-layer experiment
By W. Lance Richards
“Analytical and experimental verification of a flight article for a Mach-8 boundary-layer experiment” Metadata:
- Title: ➤ Analytical and experimental verification of a flight article for a Mach-8 boundary-layer experiment
- Author: W. Lance Richards
- Number of Pages: Median: 12
- Publisher: ➤ Dryden Flight Research Facility
- Publish Date: 1996
- Publish Location: Edwards, Calif
“Analytical and experimental verification of a flight article for a Mach-8 boundary-layer experiment” Subjects and Themes:
- Subjects: Structural analysis - Boundary layer transition
Edition Identifiers:
- The Open Library ID: OL22347312M
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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44Experiments to verify nonparallel stability theory at Virginia Polytechnic Institute and State University, Blacksburg, Virginia
By W. S. Saric
“Experiments to verify nonparallel stability theory at Virginia Polytechnic Institute and State University, Blacksburg, Virginia” Metadata:
- Title: ➤ Experiments to verify nonparallel stability theory at Virginia Polytechnic Institute and State University, Blacksburg, Virginia
- Author: W. S. Saric
- Language: English
- Publisher: ➤ Dept. of Mechanical and Aerospace Engineering, Arizona State University - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1988
- Publish Location: ➤ Springfield, Va - Tempe, Ariz - [Washington, DC
“Experiments to verify nonparallel stability theory at Virginia Polytechnic Institute and State University, Blacksburg, Virginia” Subjects and Themes:
- Subjects: ➤ Blowing - Laminar boundary layer - Perforated plates - Wind tunnel tests - Boundary layer stability - Boundary layer control - Boundary layer transition - Reynolds number suction
Edition Identifiers:
- The Open Library ID: OL15408168M
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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45Analysis of transitional separation bubbles on infinite swept wings
By R. L. Davis
“Analysis of transitional separation bubbles on infinite swept wings” Metadata:
- Title: ➤ Analysis of transitional separation bubbles on infinite swept wings
- Author: R. L. Davis
- Language: English
- Number of Pages: Median: 35
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1986
- Publish Location: ➤ [Washington, D.C.] - Springfield, Va
“Analysis of transitional separation bubbles on infinite swept wings” Subjects and Themes:
- Subjects: ➤ Inviscid flow - Viscous flow - Infinite span wings - Separated flow - Laminar flow - Aerofoils - Boundary layer transition - Bubbles - Boundary layer - Wall flow
Edition Identifiers:
- The Open Library ID: OL16116439M
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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46Boundary-layer-transition measurements in full-scale flight
By Richard D. Banner
“Boundary-layer-transition measurements in full-scale flight” Metadata:
- Title: ➤ Boundary-layer-transition measurements in full-scale flight
- Author: Richard D. Banner
- Number of Pages: Median: 10
- Publisher: ➤ National Advisory Committee for Aeronautics
- Publish Date: 1958
- Publish Location: Washington
“Boundary-layer-transition measurements in full-scale flight” Subjects and Themes:
- Subjects: Boundary layer transition
Edition Identifiers:
- The Open Library ID: OL19007435M
Access and General Info:
- First Year Published: 1958
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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47Investigations of effects of surface temperature and single roughness elements on boundary-layer transition
By Hans W. Liepmann
“Investigations of effects of surface temperature and single roughness elements on boundary-layer transition” Metadata:
- Title: ➤ Investigations of effects of surface temperature and single roughness elements on boundary-layer transition
- Author: Hans W. Liepmann
- Number of Pages: Median: 12
- Publisher: ➤ National Advisory Committee for Aeronautics
- Publish Date: 1947
- Publish Location: Washington
“Investigations of effects of surface temperature and single roughness elements on boundary-layer transition” Subjects and Themes:
- Subjects: Boundary layer transition
Edition Identifiers:
- The Open Library ID: OL19007512M
Access and General Info:
- First Year Published: 1947
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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48Analysis of the leading edge effects on the boundary layer transition
By P. L. Chow
“Analysis of the leading edge effects on the boundary layer transition” Metadata:
- Title: ➤ Analysis of the leading edge effects on the boundary layer transition
- Author: P. L. Chow
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1990
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Analysis of the leading edge effects on the boundary layer transition” Subjects and Themes:
- Subjects: ➤ Feedback control - Boundary layer transition - Boundary layer control - Aerodynamic heating - Leading edges - Active control - Optimal control - Shear flow
Edition Identifiers:
- The Open Library ID: OL15405512M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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49Longitudinal aerodynamic characteristics of a subsonic, energy-efficient transport configuration in the National Transonic Facility
By Peter F. Jacobs
“Longitudinal aerodynamic characteristics of a subsonic, energy-efficient transport configuration in the National Transonic Facility” Metadata:
- Title: ➤ Longitudinal aerodynamic characteristics of a subsonic, energy-efficient transport configuration in the National Transonic Facility
- Author: Peter F. Jacobs
- Language: English
- Number of Pages: Median: 67
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
- Publish Date: 1989
- Publish Location: [Washington, D.C.]
“Longitudinal aerodynamic characteristics of a subsonic, energy-efficient transport configuration in the National Transonic Facility” Subjects and Themes:
- Subjects: ➤ Transport planes - Nonadiabatic conditions - Longitudinal stability - Subsonic speed - Wall temperature - Boundary layer transition - Aeroelasticity - Supercritical wings
Edition Identifiers:
- The Open Library ID: OL16135206M
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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Downloads Are Not Available:
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50Experimental evaluation of the effect of angle-of-attack on the external aerodynamics and mass capture of a symmetric three-engine air-breathing launch vehicle configuration at supersonic speeds
By Hyun D. Kim
“Experimental evaluation of the effect of angle-of-attack on the external aerodynamics and mass capture of a symmetric three-engine air-breathing launch vehicle configuration at supersonic speeds” Metadata:
- Title: ➤ Experimental evaluation of the effect of angle-of-attack on the external aerodynamics and mass capture of a symmetric three-engine air-breathing launch vehicle configuration at supersonic speeds
- Author: Hyun D. Kim
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - Available from NASA Center for Aerospace Information
- Publish Date: 2001
- Publish Location: ➤ Hanover, MD - [Cleveland, Ohio]
“Experimental evaluation of the effect of angle-of-attack on the external aerodynamics and mass capture of a symmetric three-engine air-breathing launch vehicle configuration at supersonic speeds” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Dimensional analysis - Flow distribution - Boundary layer transition - Aerodynamic characteristics - Angle of attack
Edition Identifiers:
- The Open Library ID: OL18479599M
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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