Explore: Free Flow
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Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Receptivity 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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2Improved two-equation k - [omega] turbulence models for aerodynamic flows
By Florian R. Menter
“Improved two-equation k - [omega] turbulence models for aerodynamic flows” Metadata:
- Title: ➤ Improved two-equation k - [omega] turbulence models for aerodynamic flows
- Author: Florian R. Menter
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1992
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Improved two-equation k - [omega] turbulence models for aerodynamic flows” Subjects and Themes:
- Subjects: ➤ Boundary layers - Flow distribution - Free flow - Pressure gradients - Shear layers - Shear stress - Turbulence models - Turbulent flow
Edition Identifiers:
- The Open Library ID: OL15404624M - OL17009627M - OL18076669M - OL17114103M
- Online Computer Library Center (OCLC) ID: 32333258
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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3Self-similar compressible free vortices
By Karl Von Ellenrieder
“Self-similar compressible free vortices” Metadata:
- Title: ➤ Self-similar compressible free vortices
- Author: Karl Von Ellenrieder
- Language: English
- Publisher: ➤ Joint Institute for Aeronautics and Acoustics, Stanford University - National Technical Information Service, distributor - Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1998
- Publish Location: ➤ [Springfield, Va - [Stanford, Calif.]
“Self-similar compressible free vortices” Subjects and Themes:
- Subjects: ➤ Lie groups - Numerical analysis - Perturbation - Vorticity - Vortices - Mathematical models - Two dimensional flow - Axisymmetric flow - Prandtl number - Navier-Stokes equation - Incompressible flow - Free flow
Edition Identifiers:
- The Open Library ID: OL17581926M - OL15545013M - OL17131181M - OL18133565M
- Online Computer Library Center (OCLC) ID: 41414290
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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4The 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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5Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction
By Aerospace Sciences Meeting & Exhibit (32nd 1994 Reno, Nev.)
“Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction” Metadata:
- Title: ➤ Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction
- Author: ➤ Aerospace Sciences Meeting & Exhibit (32nd 1994 Reno, Nev.)
- Language: English
- Publisher: ➤ American Institute of Aeronautics and Astronautics - [National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ Springfield, Va - Washington, D.C
“Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction” Subjects and Themes:
- Subjects: Boundary layers - Free flow - Skin friction - Supersonic speed - Turbulence models
Edition Identifiers:
- The Open Library ID: OL17135643M - OL18138002M - OL17593576M - OL15557726M
- Online Computer Library Center (OCLC) ID: 42817199
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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6Pitot-pressure measurements in flow fields behind a rectangular nozzle with exhaust jet for free-stream mach numbers of 0.00, 0,60, and 1.20
By Lawrence E. Putnam
“Pitot-pressure measurements in flow fields behind a rectangular nozzle with exhaust jet for free-stream mach numbers of 0.00, 0,60, and 1.20” Metadata:
- Title: ➤ Pitot-pressure measurements in flow fields behind a rectangular nozzle with exhaust jet for free-stream mach numbers of 0.00, 0,60, and 1.20
- Author: Lawrence E. Putnam
- Language: English
- Number of Pages: Median: 151
- Publisher: ➤ National Technical Information Service, distributor] - Langley Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1986
- Publish Location: ➤ [Washington, DC] - [Springfield, Va - Hampton, Va
“Pitot-pressure measurements in flow fields behind a rectangular nozzle with exhaust jet for free-stream mach numbers of 0.00, 0,60, and 1.20” Subjects and Themes:
- Subjects: ➤ Exhaust nozzles - Flow distribution - Free flow - Jet exhaust - Mach number - Nozzles - Pitot tubes - Pressure measurement - Transonic speed
Edition Identifiers:
- The Open Library ID: OL20985250M - OL18083203M - OL15417483M
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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7Viscous-flow analysis of a subsonic transport aircraft high-lift system and correlation with flight data
By R. C. Potter
“Viscous-flow analysis of a subsonic transport aircraft high-lift system and correlation with flight data” Metadata:
- Title: ➤ Viscous-flow analysis of a subsonic transport aircraft high-lift system and correlation with flight data
- Author: R. C. Potter
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Dept. of Mechanical and Aeronautical Engineering, University of California
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC - Springfield, Va - Davis, CA
“Viscous-flow analysis of a subsonic transport aircraft high-lift system and correlation with flight data” Subjects and Themes:
- Subjects: ➤ Airfoil profiles - Computational grids - Flight tests - Free flow - Navier-Stokes equation - Performance prediction - Swept wings - Three dimensional flow - Transition flow - Two dimensional flow - Viscous flow - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15418997M - OL18084407M - OL17076220M
- Online Computer Library Center (OCLC) ID: 34776510
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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8Separation characteristics of generic stores from lee side of an inclined flat plate at Mach 6
By Floyd J. Wilcox
“Separation characteristics of generic stores from lee side of an inclined flat plate at Mach 6” Metadata:
- Title: ➤ Separation characteristics of generic stores from lee side of an inclined flat plate at Mach 6
- Author: Floyd J. Wilcox
- Language: English
- Number of Pages: Median: 43
- Publisher: ➤ Available from the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center - For sale by the National Technical Information Service
- Publish Date: 1995
- Publish Location: ➤ Hampton, Va - Springfield, VA - [Springfield, VA
“Separation characteristics of generic stores from lee side of an inclined flat plate at Mach 6” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Aerodynamics, Hypersonic - Bombers - Design and construction - External store separation - External stores - Flat plates - Free flow - Hypersonic Aerodynamics - Hypersonic speed - Separated flow
Edition Identifiers:
- The Open Library ID: OL17635043M - OL16125421M - OL17803983M
- Online Computer Library Center (OCLC) ID: 60398151 - 33144596
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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9The unsteady laminar boundary layer on an axisymmetric body subject to small amplitude fluctuations in the free-stream velocity
By Peter W. Duck
“The unsteady laminar boundary layer on an axisymmetric body subject to small amplitude fluctuations in the free-stream velocity” Metadata:
- Title: ➤ The unsteady laminar boundary layer on an axisymmetric body subject to small amplitude fluctuations in the free-stream velocity
- Author: Peter W. Duck
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering
- Publish Date: 1991
- Publish Location: Hampton, Va - [Springfield, Va
“The unsteady laminar boundary layer on an axisymmetric body subject to small amplitude fluctuations in the free-stream velocity” Subjects and Themes:
- Subjects: ➤ Boundary layer - Flow velocity - Free flow - Laminar boundary layer - Circular cylinders - Eigenvalues - Unsteady flow - Axisymmetric bodies
Edition Identifiers:
- The Open Library ID: OL16123848M - OL17633047M
- Online Computer Library Center (OCLC) ID: 58956979
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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10Detailed flow-field measurements over a 75⁰ swept delta wing
By Scott O. Kjelgaard
“Detailed flow-field measurements over a 75⁰ swept delta wing” Metadata:
- Title: ➤ Detailed flow-field measurements over a 75⁰ swept delta wing
- Author: Scott O. Kjelgaard
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - National Technical Information Service, distributor]
- Publish Date: 1990
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Detailed flow-field measurements over a 75⁰ swept delta wing” Subjects and Themes:
- Subjects: ➤ Vortices - Delta wings - Swept wing - Flow visualization - Jet flow - Free flow - Flow distribution
Edition Identifiers:
- The Open Library ID: OL18077244M - OL15405497M
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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11Pressure distributions from subsonic tests of a NACA 0012 semispan wing model
By Zachary T. Applin
“Pressure distributions from subsonic tests of a NACA 0012 semispan wing model” Metadata:
- Title: ➤ Pressure distributions from subsonic tests of a NACA 0012 semispan wing model
- Author: Zachary T. Applin
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: Hampton, Va - [Springfield, Va
“Pressure distributions from subsonic tests of a NACA 0012 semispan wing model” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Airfoil profiles - Dynamic pressure - Free flow - Pressure distribution - Semispan models - Subsonic speed - Unswept wings - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15421506M - OL17794166M
- Online Computer Library Center (OCLC) ID: 35231688
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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12Summary report of the orbital X-34 wing static aeroelastic study
By Ramadas K. Prabhu
“Summary report of the orbital X-34 wing static aeroelastic study” Metadata:
- Title: ➤ Summary report of the orbital X-34 wing static aeroelastic study
- Author: Ramadas K. Prabhu
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Science Administration, Langley Research Center
- Publish Date: 2001
- Publish Location: Hampton, Va - Hanover, MD
“Summary report of the orbital X-34 wing static aeroelastic study” Subjects and Themes:
- Subjects: ➤ Inviscid flow - Computational fluid dynamics - Free flow - X-34 reusable launch vehicle - Aerodynamic characteristics - Flexibility - Dynamic pressure - Aeroelasticity
Edition Identifiers:
- The Open Library ID: OL17607405M - OL16030672M
- Online Computer Library Center (OCLC) ID: 50133893
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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13Parametric study of shock-induced combustion in a hydrogen air system
By J. K. Ahuja
“Parametric study of shock-induced combustion in a hydrogen air system” Metadata:
- Title: ➤ Parametric study of shock-induced combustion in a hydrogen air system
- Author: J. K. Ahuja
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - NASA Langley Research Center - Institute for Computational and Applied Mechanics, Old Dominion University
- Publish Date: 1994
- Publish Location: ➤ Hampton, Va - Norfolk, Va - [Springfield, Va
“Parametric study of shock-induced combustion in a hydrogen air system” Subjects and Themes:
- Subjects: ➤ Combustion physics - Wave interaction - Mathematical models - Free flow - Activation energy - Blunt bodies - Hypersonic speed - Shock heating
Edition Identifiers:
- The Open Library ID: OL15409433M
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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14The influence of free-stream turbulence on turbulent boundary layers with mild adverse pressure gradients
By Jon A. Hoffmann
“The influence of free-stream turbulence on turbulent boundary layers with mild adverse pressure gradients” Metadata:
- Title: ➤ The influence of free-stream turbulence on turbulent boundary layers with mild adverse pressure gradients
- Author: Jon A. Hoffmann
- Language: English
- Publisher: ➤ Aeronautical Engineering Dept., California Polytechnic State University ; [Washington, D.C. - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1988
- Publish Location: ➤ Springfield, Va - San Luis Obispo, Calif
“The influence of free-stream turbulence on turbulent boundary layers with mild adverse pressure gradients” Subjects and Themes:
- Subjects: Pressure gradients - Turbulent boundary layer - Free flow - Isotropic turbulence
Edition Identifiers:
- The Open Library ID: OL18079291M - OL15409954M
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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15Increased heat transfer to a cylindrical leading edge due to spanwise variations in the freestream velocity
By David L. Rigby
“Increased heat transfer to a cylindrical leading edge due to spanwise variations in the freestream velocity” Metadata:
- Title: ➤ Increased heat transfer to a cylindrical leading edge due to spanwise variations in the freestream velocity
- Author: David L. Rigby
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1991
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Increased heat transfer to a cylindrical leading edge due to spanwise variations in the freestream velocity” Subjects and Themes:
- Subjects: ➤ Cylindrical bodies - Free flow - Heat transfer - Horeshoe vortices - Numerical analysis - Vorticity
Edition Identifiers:
- The Open Library ID: OL17682418M
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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16Receptivity 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
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: Hampton, Va - [Springfield, Va
“Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate)” Subjects and Themes:
- Subjects: ➤ Boundary layers - Vorticity - Wakes - Leading edges - Free flow - Flat plates
Edition Identifiers:
- The Open Library ID: OL17591434M
- Online Computer Library Center (OCLC) ID: 42623773
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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17Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream
By George C. Olsen
“Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream” Metadata:
- Title: ➤ Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream
- Author: George C. Olsen
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream” Subjects and Themes:
- Subjects: ➤ Hypersonic flow - Cold flow tests - Free flow - Supersonic combustion ramjet engines - Film cooling - Mass flow rate - Coolants - Oblique shock waves - Thermal protection - Gas flow - Two dimensional models - Hydrogen - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15416715M
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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18Influence of turbulence parameters, Reynolds number, and body shape on stagnation-region heat transfer
By G. James VanFossen
“Influence of turbulence parameters, Reynolds number, and body shape on stagnation-region heat transfer” Metadata:
- Title: ➤ Influence of turbulence parameters, Reynolds number, and body shape on stagnation-region heat transfer
- Author: G. James VanFossen
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1994
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Influence of turbulence parameters, Reynolds number, and body shape on stagnation-region heat transfer” Subjects and Themes:
- Subjects: ➤ Turbulent flow - Heat flux - Liminar heat transfer - Mathematical models - Wind tunnel tests - Free flow - Stagnation flow - Shapes - Reynolds number - Atmospheric turbulence - Turbulence effects
Edition Identifiers:
- The Open Library ID: OL15413563M
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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19Towards enhancing and delaying disturbances in free shear flows
By William O. Criminale
“Towards enhancing and delaying disturbances in free shear flows” Metadata:
- Title: ➤ Towards enhancing and delaying disturbances in free shear flows
- Author: William O. Criminale
- Language: English
- Publisher: ➤ Institute for Computer Applications in Science and Engineering, NASA Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: Hampton, Va - [Springfield, Va
“Towards enhancing and delaying disturbances in free shear flows” Subjects and Themes:
- Subjects: ➤ Inviscid flow - Mixing layers (Fluids) - Wakes - Jet flow - Free flow - Incompressible fluids - Flow stability - Shear flow
Edition Identifiers:
- The Open Library ID: OL17682547M
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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20Artificial boundary conditions for computation of oscillating external flows
By S. V. Tsynkov
“Artificial boundary conditions for computation of oscillating external flows” Metadata:
- Title: ➤ Artificial boundary conditions for computation of oscillating external flows
- Author: S. V. Tsynkov
- 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
“Artificial boundary conditions for computation of oscillating external flows” Subjects and Themes:
- Subjects: ➤ Viscous flow - Oscillating flow - Free flow - Finite difference theory - Navier-Stokes equation - Airfoils - Boundary conditions - Compressible flow
Edition Identifiers:
- The Open Library ID: OL15504608M
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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21Jet vortex generators for turbulent flow separation control
By Gregory V. Selby
“Jet vortex generators for turbulent flow separation control” Metadata:
- Title: ➤ Jet vortex generators for turbulent flow separation control
- Author: Gregory V. Selby
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - Old Dominion University Research Foundation - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1990
- Publish Location: ➤ [Springfield, Va - Hampton, Va - Norfolk, Va
“Jet vortex generators for turbulent flow separation control” Subjects and Themes:
- Subjects: ➤ Vortex generators - Boundary layer control - Boundary layer separation - Jet flow - Free flow - Flow distribution
Edition Identifiers:
- The Open Library ID: OL16129968M
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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22Magellan aerodynamic characteristics during the termination experiment including thruster plume-free stream interaction
By Francisco J. Cestero
“Magellan aerodynamic characteristics during the termination experiment including thruster plume-free stream interaction” Metadata:
- Title: ➤ Magellan aerodynamic characteristics during the termination experiment including thruster plume-free stream interaction
- Author: Francisco J. Cestero
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1998
- Publish Location: Hampton, Va - [Springfield, Va
“Magellan aerodynamic characteristics during the termination experiment including thruster plume-free stream interaction” Subjects and Themes:
- Subjects: ➤ Exhaust gases - Turbulent flow - Magellan spacecraft (NASA) - Plumes - Aerodynamic characteristics - Free flow - Thrust reversal
Edition Identifiers:
- The Open Library ID: OL15543650M
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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23Transitional boundary layers under the influence of high free stream turbulence, intensive wall cooling and high pressure gradinets in hot gas circulation
By Klaus Rued
“Transitional boundary layers under the influence of high free stream turbulence, intensive wall cooling and high pressure gradinets in hot gas circulation” Metadata:
- Title: ➤ Transitional boundary layers under the influence of high free stream turbulence, intensive wall cooling and high pressure gradinets in hot gas circulation
- Author: Klaus Rued
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1987
- Publish Location: ➤ Washington, D. C - [Springfield, Va
“Transitional boundary layers under the influence of high free stream turbulence, intensive wall cooling and high pressure gradinets in hot gas circulation” Subjects and Themes:
- Subjects: ➤ Surface cooling - Turbulent boundary layer - Boundary layer transition - Pressure gradients - Gas flow - Free flow
Edition Identifiers:
- The Open Library ID: OL15417348M
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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24Comparison of turbulence models for nozzle-afterbody flows with propulsive jets
By William B. Compton
“Comparison of turbulence models for nozzle-afterbody flows with propulsive jets” Metadata:
- Title: ➤ Comparison of turbulence models for nozzle-afterbody flows with propulsive jets
- Author: William B. Compton
- 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
“Comparison of turbulence models for nozzle-afterbody flows with propulsive jets” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Angle of attack - Axisymmetric flow - Computational fluid dynamics - Convergent-divergent nozzles - Exhaust gases - Free flow - Jet exhaust - K-epsilon turbulence model - Navier-Stokes equation - Nozzle flow - Turbulence models
Edition Identifiers:
- The Open Library ID: OL15504433M
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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25Effect of curvature on the impact damage characteritiscs and residual strength of composite plates
By Damodar R. Ambur
“Effect of curvature on the impact damage characteritiscs and residual strength of composite plates” Metadata:
- Title: ➤ Effect of curvature on the impact damage characteritiscs and residual strength of composite plates
- Author: Damodar R. Ambur
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Effect of curvature on the impact damage characteritiscs and residual strength of composite plates” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Tangential blowing - Analysis (Mathematics) - Slots - Free flow - Forebodies - Yawing moments
Edition Identifiers:
- The Open Library ID: OL15509443M
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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26On the interaction between the shock wave attached to a wedge and freestream disturbances
By Peter W. Duck
“On the interaction between the shock wave attached to a wedge and freestream disturbances” Metadata:
- Title: ➤ On the interaction between the shock wave attached to a wedge and freestream disturbances
- Author: Peter W. Duck
- Number of Pages: Median: 44
- Publisher: ➤ Institute for Computer Applications in Science and Engineering
- Publish Date: 1993
- Publish Location: Hampton, Va
“On the interaction between the shock wave attached to a wedge and freestream disturbances” Subjects and Themes:
- Subjects: Free flow - Shock waves
Edition Identifiers:
- The Open Library ID: OL19917272M
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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27Water tunnel flow visualization study through poststall of 12 novel planform shapes
By Gregory M. Gatlin
“Water tunnel flow visualization study through poststall of 12 novel planform shapes” Metadata:
- Title: ➤ Water tunnel flow visualization study through poststall of 12 novel planform shapes
- Author: Gregory M. Gatlin
- 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
“Water tunnel flow visualization study through poststall of 12 novel planform shapes” Subjects and Themes:
- Subjects: ➤ Planforms - Water tunnel tests - Flow visualization - Aerodynamic configurations - Free flow - Wing profiles - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15503578M
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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28On the freestream matching condition for stagnation point turbulent flows
By C. G. Speziale
“On the freestream matching condition for stagnation point turbulent flows” Metadata:
- Title: ➤ On the freestream matching condition for stagnation point turbulent flows
- Author: C. G. Speziale
- Language: English
- Publisher: ➤ Institute for Computer Applications in Science and Engineering, NASA Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1989
- Publish Location: [Springfield, Va - Hampton, VA
“On the freestream matching condition for stagnation point turbulent flows” Subjects and Themes:
- Subjects: Plane strain - Stagnation point - Free flow - Turbulent flow
Edition Identifiers:
- The Open Library ID: OL15407381M
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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29Effect of surface waviness on transition in three-dimensional boundary-layer flow
By Jamal A. Masad
“Effect of surface waviness on transition in three-dimensional boundary-layer flow” Metadata:
- Title: ➤ Effect of surface waviness on transition in three-dimensional boundary-layer flow
- Author: Jamal A. Masad
- 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
“Effect of surface waviness on transition in three-dimensional boundary-layer flow” Subjects and Themes:
- Subjects: ➤ Free flow - Surface waves - Boundary layer transition - Three dimensional boundary layer - Three dimensional flow - Transition flow
Edition Identifiers:
- The Open Library ID: OL15505112M
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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30Hypersonic flows about a 25 ̊sharp cone
By James N. Moss
“Hypersonic flows about a 25 ̊sharp cone” Metadata:
- Title: ➤ Hypersonic flows about a 25 ̊sharp cone
- Author: James N. Moss
- Language: English
- Publisher: ➤ Available from NASA Center for AeroSpace Information (CASI) - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 2001
- Publish Location: Hampton, Va - Hanover MD
“Hypersonic flows about a 25 ̊sharp cone” Subjects and Themes:
- Subjects: ➤ Slender cones - Numeral analysis - Temperature profiles - Computerized simulation - Shock tunnels - Hypersonic flow - Free flow
Edition Identifiers:
- The Open Library ID: OL16046877M
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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31The effect of vortex generators on a jet in a cross-flow
By K. B. M. Q. Zaman
“The effect of vortex generators on a jet in a cross-flow” Metadata:
- Title: ➤ The effect of vortex generators on a jet in a cross-flow
- Author: K. B. M. Q. Zaman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - American Institute of Physics - National Technical Information Service, distributor]
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, D.C - [Woodbury, NY]
“The effect of vortex generators on a jet in a cross-flow” Subjects and Themes:
- Subjects: ➤ Vortex generators - Jet flow - Pressure distribution - Cross flow - Free flow - Flow distribution - Penetration - Free jets - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15541866M
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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32Exploratory flow visualization investigation of mast-mounted sights in presence of a rotor
By Terence A. Ghee
“Exploratory flow visualization investigation of mast-mounted sights in presence of a rotor” Metadata:
- Title: ➤ Exploratory flow visualization investigation of mast-mounted sights in presence of a rotor
- Author: Terence A. Ghee
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - US Army Aviation Systems Command, Aviation R&T Activity
- Publish Date: 1995
- Publish Location: Hampton, Va - [St. Louis, Mo.]
“Exploratory flow visualization investigation of mast-mounted sights in presence of a rotor” Subjects and Themes:
- Subjects: ➤ Flow visualization - Vibration - Aerodynamic characteristics - Rotors - Wind tunnel tests - Free flow - Flow distribution
Edition Identifiers:
- The Open Library ID: OL17115724M
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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33A new methodology for free wake analysis using curved vortex elements
By Donald B. Bliss
“A new methodology for free wake analysis using curved vortex elements” Metadata:
- Title: ➤ A new methodology for free wake analysis using curved vortex elements
- Author: Donald B. Bliss
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1987
- Publish Location: [Washington, D.C.]
“A new methodology for free wake analysis using curved vortex elements” Subjects and Themes:
- Subjects: ➤ Free flow - Vortex filaments - Vortices - Helicopter wakes - Rotor aerodynamics - Rotary wings - Downwash - Rotors
Edition Identifiers:
- The Open Library ID: OL16133036M
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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34Measurements in transitional boundary layers under high free-stream turbulence and strong acceleration conditions
By Ralph J. Volino
“Measurements in transitional boundary layers under high free-stream turbulence and strong acceleration conditions” Metadata:
- Title: ➤ Measurements in transitional boundary layers under high free-stream turbulence and strong acceleration conditions
- Author: Ralph J. Volino
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Measurements in transitional boundary layers under high free-stream turbulence and strong acceleration conditions” Subjects and Themes:
- Subjects: ➤ Velocity distribution - Turbulent heat transfer - Temperature profiles - Boundary layer transition - Flow characteristics - Free flow - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15539477M
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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35Demonstration of the feasibility of laser induced fluorescence for arc jet flow diagnostics
By Sivaram Arepalli
“Demonstration of the feasibility of laser induced fluorescence for arc jet flow diagnostics” Metadata:
- Title: ➤ Demonstration of the feasibility of laser induced fluorescence for arc jet flow diagnostics
- Author: Sivaram Arepalli
- Language: English
- Publisher: ➤ Structures and Mechanics Division and Advanced Programs Office, National Aeronautics and Space Administration, Lyndon B. Johnson Space Center - Lockheed Engineering and Sciences Company
- Publish Date: 1989
- Publish Location: Houston, Tex
“Demonstration of the feasibility of laser induced fluorescence for arc jet flow diagnostics” Subjects and Themes:
- Subjects: ➤ Blunt bodies - Diagnosis - Jet flow - Laser induced fluoescence - Free flow - Shock layers
Edition Identifiers:
- The Open Library ID: OL16143529M
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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