Explore: Reynolds Number
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AI-Generated Overview About “reynolds-number”:
Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1A near-wall Reynolds-stress closure without wall normals
By S. P. Yuan
“A near-wall Reynolds-stress closure without wall normals” Metadata:
- Title: ➤ A near-wall Reynolds-stress closure without wall normals
- Author: S. P. Yuan
- Language: English
- Number of Pages: Median: 263
- Publisher: ➤ College of Engineering and Applied Sciences, Arizona State University - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, DC - Tempe, Ariz - Springfield, Va
“A near-wall Reynolds-stress closure without wall normals” Subjects and Themes:
- Subjects: ➤ Reynolds stress - Stress analysis - Reynolds number - Turbulence - Mathematical models - High Reynolds number - Boundary layer flow - Wall flow - Channel flow - Secondary flow - Three dimensional flow - Walls - Coriolis effect - Pipe flow - Boundary value problems - Turbulent boundary layer - Aerodynamics
Edition Identifiers:
- The Open Library ID: ➤ OL17564635M - OL17124019M - OL18114320M - OL17576384M - OL17126655M - OL15504980M - OL18121465M - OL19141393M - OL15486046M
- Online Computer Library Center (OCLC) ID: 40265766 - 39341768
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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2Aerodynamics of low reynolds number flyers
By Wei Shyy
“Aerodynamics of low reynolds number flyers” Metadata:
- Title: ➤ Aerodynamics of low reynolds number flyers
- Author: Wei Shyy
- Language: English
- Number of Pages: Median: 196
- Publisher: Cambridge University Press
- Publish Date: 2007 - 2008 - 2009 - 2011
- Publish Location: Cambridge - New York
“Aerodynamics of low reynolds number flyers” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Birds, flight - Flying-machines - Ornithopters - Birds - Flight - Reynolds number
Edition Identifiers:
- The Open Library ID: ➤ OL40621412M - OL40469441M - OL40378231M - OL34444308M - OL28467461M - OL17915648M - OL10438403M - OL17246025M
- Online Computer Library Center (OCLC) ID: 190785883
- Library of Congress Control Number (LCCN): 2007019227
- All ISBNs: ➤ 9780511477195 - 0521882788 - 0511551150 - 0521204011 - 9780521882781 - 0511478712 - 0511477198 - 9780511478710 - 9780511551154 - 0511473923 - 9780511473920 - 9780521204019
Access and General Info:
- First Year Published: 2007
- Is Full Text Available: Yes
- Is The Book Public: No
- Access Status: Printdisabled
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3Hot-jet simulation in cryogenic wind tunnels
By Keisuke Asai
“Hot-jet simulation in cryogenic wind tunnels” Metadata:
- Title: ➤ Hot-jet simulation in cryogenic wind tunnels
- Author: Keisuke Asai
- Language: English
- Number of Pages: Median: 45
- Publisher: ➤ For sale by the National Technical Information Service] - Langley Research Center - National Aeronautics and SpaceAdministration - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
- Publish Date: 1989
- Publish Location: ➤ Washington D.C - Hampton, Va - Washington, D.C - [Springfield, Va - [Washington, DC]
“Hot-jet simulation in cryogenic wind tunnels” Subjects and Themes:
- Subjects: ➤ Cryogenic wind tunnels - Exhaust flow simulation - Jet flow - Reynolds number - Wind tunnel tests - Wind tunnels
Edition Identifiers:
- The Open Library ID: ➤ OL17683287M - OL19959189M - OL13931490M - OL15576426M - OL18208937M - OL19379736M - OL18078046M - OL1812959M
- Online Computer Library Center (OCLC) ID: 20034307
- Library of Congress Control Number (LCCN): 89602567
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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4Assessment 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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5Low-speed aerodynamic characteristics of a 1/8-scale X-29A airplane model at high angles of attack and side slip
By Raymond D. Whipple
“Low-speed aerodynamic characteristics of a 1/8-scale X-29A airplane model at high angles of attack and side slip” Metadata:
- Title: ➤ Low-speed aerodynamic characteristics of a 1/8-scale X-29A airplane model at high angles of attack and side slip
- Author: Raymond D. Whipple
- Language: English
- Number of Pages: Median: 286
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - Langley Research Center - For sale by the National Technical Information Service]
- Publish Date: 1986
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, DC]
“Low-speed aerodynamic characteristics of a 1/8-scale X-29A airplane model at high angles of attack and side slip” Subjects and Themes:
- Subjects: Reynolds number - Grumman X-29A (Jet plane) - Forebodies - Swept wings - Angle of attack
Edition Identifiers:
- The Open Library ID: OL17095022M - OL14662026M - OL18028050M - OL20984630M - OL15272847M
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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6Receptivity 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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7The boundary layer on compressor cascade blades
By Steven Deutsch
“The boundary layer on compressor cascade blades” Metadata:
- Title: ➤ The boundary layer on compressor cascade blades
- Author: Steven Deutsch
- Language: English
- Publisher: ➤ Applied Research Laboratory, The Pennsylvania State University - National Aeronautics and Space Administration
- Publish Date: 1984
- Publish Location: ➤ [Washington, D.C - State College, PA
“The boundary layer on compressor cascade blades” Subjects and Themes:
- Subjects: ➤ Airfoils - Boundary layer control - Cascades (Fluid dynamics) - Flow distribution - Laser Doppler velocimeters - Reynolds number
Edition Identifiers:
- The Open Library ID: OL17666140M - OL17727387M - OL14928515M - OL17831614M
Access and General Info:
- First Year Published: 1984
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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8Spin-tunnel investigation of a 1/28-scale model of the NASA F-18 High Alpha Research Vehicle (HARV) with and without vertical tails
By Charles Michael Fremaux
“Spin-tunnel investigation of a 1/28-scale model of the NASA F-18 High Alpha Research Vehicle (HARV) with and without vertical tails” Metadata:
- Title: ➤ Spin-tunnel investigation of a 1/28-scale model of the NASA F-18 High Alpha Research Vehicle (HARV) with and without vertical tails
- Author: Charles Michael Fremaux
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - For sale by the National Technical Information Service
- Publish Date: 1997
- Publish Location: [Springfield, Va - Hampton, Va
“Spin-tunnel investigation of a 1/28-scale model of the NASA F-18 High Alpha Research Vehicle (HARV) with and without vertical tails” Subjects and Themes:
- Subjects: Reynolds number - Wind tunnel tests - Research vehicles - Tail assemblies - Spin tests
Edition Identifiers:
- The Open Library ID: OL17834292M - OL18114842M - OL17123433M - OL15487251M
- Online Computer Library Center (OCLC) ID: 39098301
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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9On the modeling of low-Reynolds-number turbulence
By Ronald M. C. So
“On the modeling of low-Reynolds-number turbulence” Metadata:
- Title: ➤ On the modeling of low-Reynolds-number turbulence
- Author: Ronald M. C. So
- Language: English
- Number of Pages: Median: 135
- Publisher: ➤ Lewis Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
- Publish Date: 1986
- Publish Location: ➤ [Washington, DC] - Cleveland, Ohio - [Springfield, Va
“On the modeling of low-Reynolds-number turbulence” Subjects and Themes:
- Subjects: Reynolds number - Turbulence - Turbulent flow - Low Reynolds number - Reynolds stress
Edition Identifiers:
- The Open Library ID: OL18029516M - OL20982570M - OL17659097M - OL17836871M
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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10Reynolds-averaged Navier-Stokes studies of low Reynolds number effects on the losses in a low pressure turbine
By Daniel J. Dorney
“Reynolds-averaged Navier-Stokes studies of low Reynolds number effects on the losses in a low pressure turbine” Metadata:
- Title: ➤ Reynolds-averaged Navier-Stokes studies of low Reynolds number effects on the losses in a low pressure turbine
- Author: Daniel J. Dorney
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Reynolds-averaged Navier-Stokes studies of low Reynolds number effects on the losses in a low pressure turbine” Subjects and Themes:
- Subjects: ➤ Blade-vortex interaction - Navier-Stokes equation - Propulsive efficiency - Reynolds number - Rotor stator interactions - Turbine blades - Turbines - Unsteady aerodynamics - Unsteady flow - Wakes
Edition Identifiers:
- The Open Library ID: OL17546454M - OL18116215M - OL17123448M - OL15491903M
- Online Computer Library Center (OCLC) ID: 39109525
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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11The three-dimensional flow past a rapidly rotating circular cylinder
By James P. Denier
“The three-dimensional flow past a rapidly rotating circular cylinder” Metadata:
- Title: ➤ The three-dimensional flow past a rapidly rotating circular cylinder
- Author: James P. Denier
- Language: English
- Number of Pages: Median: 15
- Publisher: ➤ National Technical Information Service, distributor - Institute for Computer Applications in Science and Engineering - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1993
- Publish Location: Hampton, Va - [Springfield, Va
“The three-dimensional flow past a rapidly rotating circular cylinder” Subjects and Themes:
- Subjects: Reynolds number - Cylinders - Three dimensional flow - Rotating cylinders
Edition Identifiers:
- The Open Library ID: OL19916830M - OL18062884M - OL15382004M - OL14697292M
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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12Flow-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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13User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel
By Ronald H. Soeder
“User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel” Metadata:
- Title: ➤ User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel
- Author: Ronald H. Soeder
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1992 - 1995
- Publish Location: ➤ [Washington, DC - [Springfield, Va - [Washington, DC] - Springfield, Va
“User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel” Subjects and Themes:
- Subjects: ➤ Supersonic wind tunnels - Performance tests - Dynamic pressure - User manuals (Computer programs) - Reynolds number - Wind tunnel tests - Mach number
Edition Identifiers:
- The Open Library ID: OL14687584M - OL17796406M - OL15425389M - OL17677053M
- Online Computer Library Center (OCLC) ID: 35268400
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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14IUTAM Symposium on Reynolds Number Scaling in Turbulent Flow
By IUTAM Symposium on Reynolds Number Scaling in Turbulent Flow (2002 Princeton, N.J.)
“IUTAM Symposium on Reynolds Number Scaling in Turbulent Flow” Metadata:
- Title: ➤ IUTAM Symposium on Reynolds Number Scaling in Turbulent Flow
- Author: ➤ IUTAM Symposium on Reynolds Number Scaling in Turbulent Flow (2002 Princeton, N.J.)
- Language: English
- Number of Pages: Median: 324
- Publisher: Kluwer Academic - Springer
- Publish Date: 2003 - 2004
- Publish Location: ➤ Dordrecht - Boston, Mass - Boston - London
“IUTAM Symposium on Reynolds Number Scaling in Turbulent Flow” Subjects and Themes:
- Subjects: Congresses - Reynolds number - Turbulence
Edition Identifiers:
- The Open Library ID: OL22136132M - OL21802037M - OL19290894M - OL22571582M
- Online Computer Library Center (OCLC) ID: 53476813
- Library of Congress Control Number (LCCN): 2003064909
- All ISBNs: 1402017758 - 9781402017759
Access and General Info:
- First Year Published: 2003
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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15Navier-Stokes analysis of turbine blade heat transfer
By Robert J. Boyle
“Navier-Stokes analysis of turbine blade heat transfer” Metadata:
- Title: ➤ Navier-Stokes analysis of turbine blade heat transfer
- Author: Robert J. Boyle
- Language: English
- Number of Pages: Median: 19
- Publisher: ➤ NASA - For sale by the National Technical Information Service
- Publish Date: 1990
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Navier-Stokes analysis of turbine blade heat transfer” Subjects and Themes:
- Subjects: ➤ Aerothermodynamics - Blades - Heat - Heat transfer - Navier-Stokes equation - Reynolds number - Separated flow - Transmission - Turbine blades - Turbines - Vanes
Edition Identifiers:
- The Open Library ID: OL18251832M - OL17630426M - OL16132959M - OL20572886M
- Online Computer Library Center (OCLC) ID: 25311495
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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16Assessment of an Euler-interacting boundary layer method using high Reynolds number transonic transport flight data
By Daryl L. Bonhaus
“Assessment of an Euler-interacting boundary layer method using high Reynolds number transonic transport flight data” Metadata:
- Title: ➤ Assessment of an Euler-interacting boundary layer method using high Reynolds number transonic transport flight data
- Author: Daryl L. Bonhaus
- 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
“Assessment of an Euler-interacting boundary layer method using high Reynolds number transonic transport flight data” Subjects and Themes:
- Subjects: ➤ Boundary layers - High Reynolds number - Euler equations of motion - Transonic flow - Unstructured grids (Mathematics) - Wings - Laminar flow - Reynolds number - Transonic Aerodynamics - Boundary layer
Edition Identifiers:
- The Open Library ID: OL17135628M - OL18132959M - OL17598636M - OL15542776M
- Online Computer Library Center (OCLC) ID: 42814385
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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17Navier-Stokes simulation of several high-lift reference H configurations
By Wendy B. Lessard
“Navier-Stokes simulation of several high-lift reference H configurations” Metadata:
- Title: ➤ Navier-Stokes simulation of several high-lift reference H configurations
- Author: Wendy B. Lessard
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service [distributor - Available from NASA Center for AeroSpace Information
- Publish Date: 1999
- Publish Location: ➤ Springfield, VA - Hampton, Va - Hanover, MD
“Navier-Stokes simulation of several high-lift reference H configurations” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Angle of attack - Body-wing configurations - Computational fluid dynamics - Navier-Stokes equation - Reynolds number - Structured grids (Mathematics) - Supersonic speed - Supersonic transports - Vortices - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15569338M - OL18140130M - OL18296120M - OL17595527M
- Online Computer Library Center (OCLC) ID: 44441535
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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18Wall-layer eruptions in turbulent flows
By J. D. A. Walker
“Wall-layer eruptions in turbulent flows” Metadata:
- Title: ➤ Wall-layer eruptions in turbulent flows
- Author: J. D. A. Walker
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - For sale by the National Technical Information Service
- Publish Date: 1990
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Wall-layer eruptions in turbulent flows” Subjects and Themes:
- Subjects: Reynolds number - Turbulence
Edition Identifiers:
- The Open Library ID: OL18030729M - OL17097399M - OL15280403M
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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19An application of a two-equation model of turbulence to three-dimensional chemically reacting flows
By J. Lee
“An application of a two-equation model of turbulence to three-dimensional chemically reacting flows” Metadata:
- Title: ➤ An application of a two-equation model of turbulence to three-dimensional chemically reacting flows
- Author: J. Lee
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1994
- Publish Location: ➤ Springfield, Va - [Washington, DC
“An application of a two-equation model of turbulence to three-dimensional chemically reacting flows” Subjects and Themes:
- Subjects: ➤ Flow distribution - K-epsilon turbulence model - Reacting flow - Reynolds number - Three dimensional flow - Turbulence effects - Turbulent flow
Edition Identifiers:
- The Open Library ID: OL15412015M - OL17008159M - OL18080109M
- Online Computer Library Center (OCLC) ID: 32984462
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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20Control of unsteady separated flow associated with the dynamic stall of airfoils
By Michael C. Wilder
“Control of unsteady separated flow associated with the dynamic stall of airfoils” Metadata:
- Title: ➤ Control of unsteady separated flow associated with the dynamic stall of airfoils
- Author: Michael C. Wilder
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - MCAT Institute
- Publish Date: 1992 - 1994 - 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC - Springfield, Va.? - San Jose, CA
“Control of unsteady separated flow associated with the dynamic stall of airfoils” Subjects and Themes:
- Subjects: ➤ Unsteady flow - Wind tunnel tests - Leading edges - Aerodynamic stalling - Boundary layer control - Unsteady flow (Aerodynamics) - Separated flow - Boundary layer separation - Reynolds number - Supercritical airfoils - Airfoil oscillations - Airfoil profiles - Airfoils - Mach number - Active control
Edition Identifiers:
- The Open Library ID: OL15365679M - OL15408283M - OL15415078M
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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21Water-tunnel study of transition flow around circular cylinders
By D. Almosnino
“Water-tunnel study of transition flow around circular cylinders” Metadata:
- Title: ➤ Water-tunnel study of transition flow around circular cylinders
- Author: D. Almosnino
- Language: English
- Number of Pages: Median: 31
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
- Publish Date: 1984
- Publish Location: ➤ [Springfield, Va - Washington, D.C
“Water-tunnel study of transition flow around circular cylinders” Subjects and Themes:
- Subjects: Reynolds number
Edition Identifiers:
- The Open Library ID: OL18037588M - OL17126888M - OL17664013M
Access and General Info:
- First Year Published: 1984
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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22Reynolds-stress and dissipation rate budgets in a turbulent channel flow
By N. N. Mansour
“Reynolds-stress and dissipation rate budgets in a turbulent channel flow” Metadata:
- Title: ➤ Reynolds-stress and dissipation rate budgets in a turbulent channel flow
- Author: N. N. Mansour
- Language: English
- Number of Pages: Median: 38
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - For sale by the National Technical Information Service
- Publish Date: 1987
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Reynolds-stress and dissipation rate budgets in a turbulent channel flow” Subjects and Themes:
- Subjects: ➤ Turbulent flow - Reynolds number - Reynolds stress - Models - Channel flow - Energy budgets - Turbulence - Dissipation
Edition Identifiers:
- The Open Library ID: OL15409048M - OL18078859M - OL17114657M
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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23High-resolution liquid crystal heat transfer measurements on the end wall of a turbine passage with variations in Reynolds number
By Steven A. Hippensteele
“High-resolution liquid crystal heat transfer measurements on the end wall of a turbine passage with variations in Reynolds number” Metadata:
- Title: ➤ High-resolution liquid crystal heat transfer measurements on the end wall of a turbine passage with variations in Reynolds number
- Author: Steven A. Hippensteele
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - For sale by the National Technical Information Service
- Publish Date: 1989
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“High-resolution liquid crystal heat transfer measurements on the end wall of a turbine passage with variations in Reynolds number” Subjects and Themes:
- Subjects: Transmission - Reynolds number - Heat
Edition Identifiers:
- The Open Library ID: OL17096580M - OL15277012M - OL18029847M
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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24Low-speed tests of a high-aspect-ratio, supercritical-wing transport model equipped with a high-lift flap system in the Langley 4- by 7-meter and Ames 12-foot pressure tunnels
By Harry L. Morgan
“Low-speed tests of a high-aspect-ratio, supercritical-wing transport model equipped with a high-lift flap system in the Langley 4- by 7-meter and Ames 12-foot pressure tunnels” Metadata:
- Title: ➤ Low-speed tests of a high-aspect-ratio, supercritical-wing transport model equipped with a high-lift flap system in the Langley 4- by 7-meter and Ames 12-foot pressure tunnels
- Author: Harry L. Morgan
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - National Technical Information Service, distributor]
- Publish Date: 1983
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Low-speed tests of a high-aspect-ratio, supercritical-wing transport model equipped with a high-lift flap system in the Langley 4- by 7-meter and Ames 12-foot pressure tunnels” Subjects and Themes:
- Subjects: Reynolds number - Aerodynamics
Edition Identifiers:
- The Open Library ID: OL15393888M - OL18069134M - OL18347440M
Access and General Info:
- First Year Published: 1983
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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25A study of high-lift airfoils at high Reynolds numbers in the Langley Low-Turbulence Pressure Tunnel
By Harry L. Morgan
“A study of high-lift airfoils at high Reynolds numbers in the Langley Low-Turbulence Pressure Tunnel” Metadata:
- Title: ➤ A study of high-lift airfoils at high Reynolds numbers in the Langley Low-Turbulence Pressure Tunnel
- Author: Harry L. Morgan
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1989
- Publish Location: [Washington, DC]
“A study of high-lift airfoils at high Reynolds numbers in the Langley Low-Turbulence Pressure Tunnel” Subjects and Themes:
- Subjects: Reynolds number - Aerofoils
Edition Identifiers:
- The Open Library ID: OL15279481M - OL17097122M - OL18030455M
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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26Static aerodynamic characteristics of a typical single-engine low-wing general aviation design for an angle-of-attack range of - 8 ̊to 90 ̊
By William Bihrle
“Static aerodynamic characteristics of a typical single-engine low-wing general aviation design for an angle-of-attack range of - 8 ̊to 90 ̊” Metadata:
- Title: ➤ Static aerodynamic characteristics of a typical single-engine low-wing general aviation design for an angle-of-attack range of - 8 ̊to 90 ̊
- Author: William Bihrle
- Language: English
- Number of Pages: Median: 464
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Office - for sale by the National Technical Information Service
- Publish Date: 1978
- Publish Location: Washington - Springfield, Va
“Static aerodynamic characteristics of a typical single-engine low-wing general aviation design for an angle-of-attack range of - 8 ̊to 90 ̊” Subjects and Themes:
- Subjects: Reynolds number - Airplanes - Wings - Spin (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL17648016M - OL17818653M - OL14930027M
Access and General Info:
- First Year Published: 1978
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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27Transonic Navier-Stokes calculations about a 65⁰ delta wing
By W. Kelly Londenberg
“Transonic Navier-Stokes calculations about a 65⁰ delta wing” Metadata:
- Title: ➤ Transonic Navier-Stokes calculations about a 65⁰ delta wing
- Author: W. Kelly Londenberg
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1994
- Publish Location: Hampton, Va - [Springfield, Va
“Transonic Navier-Stokes calculations about a 65⁰ delta wing” Subjects and Themes:
- Subjects: ➤ Delta wings - Leading edges - Vortices - Reynolds number - Transonic flow - Turbulence models
Edition Identifiers:
- The Open Library ID: OL18079111M - OL15409447M - OL17790639M
- Online Computer Library Center (OCLC) ID: 32771918
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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28Final report for the grant integration of viscous effects into inviscid computational methods
By Katz, Joseph
“Final report for the grant integration of viscous effects into inviscid computational methods” Metadata:
- Title: ➤ Final report for the grant integration of viscous effects into inviscid computational methods
- Author: Katz, Joseph
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1990
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Final report for the grant integration of viscous effects into inviscid computational methods” Subjects and Themes:
- Subjects: Reynolds number
Edition Identifiers:
- The Open Library ID: OL14697049M - OL17679579M
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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29Instability 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
Online Access
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30Velocity-pressure integrated versus penalty finite element methods for high Reynolds number flows
By Sang-Wook Kim
“Velocity-pressure integrated versus penalty finite element methods for high Reynolds number flows” Metadata:
- Title: ➤ Velocity-pressure integrated versus penalty finite element methods for high Reynolds number flows
- Author: Sang-Wook Kim
- Language: English
- Publisher: ➤ For sale by National Technical Information Service - NASA-Marshall Space Flight Center
- Publish Date: 1988
- Publish Location: ➤ [Springfield, Va - Marshall Space Flight Center, Ala
“Velocity-pressure integrated versus penalty finite element methods for high Reynolds number flows” Subjects and Themes:
- Subjects: Reynolds number - Finite element method
Edition Identifiers:
- The Open Library ID: OL18031782M - OL15284666M
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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31The effects of viscosity on the stability of a trailing-line vortex in compressible flow
By Jillian A. K. Stott
“The effects of viscosity on the stability of a trailing-line vortex in compressible flow” Metadata:
- Title: ➤ The effects of viscosity on the stability of a trailing-line vortex in compressible flow
- Author: Jillian A. K. Stott
- 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: [Springfield, Va - Hampton, VA
“The effects of viscosity on the stability of a trailing-line vortex in compressible flow” Subjects and Themes:
- Subjects: ➤ Viscous flow - Compressible flow - Vortices - Reynolds number - Viscosity - Mach number - Flow stability
Edition Identifiers:
- The Open Library ID: OL15404287M - OL17790339M
- Online Computer Library Center (OCLC) ID: 32296404
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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32Numerical simulation of internal heat transfer phenomena occurring during de-icing of aircraft components
By Kenneth J. De Witt
“Numerical simulation of internal heat transfer phenomena occurring during de-icing of aircraft components” Metadata:
- Title: ➤ Numerical simulation of internal heat transfer phenomena occurring during de-icing of aircraft components
- Author: Kenneth J. De Witt
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Numerical simulation of internal heat transfer phenomena occurring during de-icing of aircraft components” Subjects and Themes:
- Subjects: ➤ Stanton number - Convective heat transfer - Reynolds number - Heat transfer coefficients - Surface roughness - Ice formation - Mathematical models - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17834312M - OL15487146M
- Online Computer Library Center (OCLC) ID: 39218132
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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33Performance analysis of two early NACA high speed propellers with application to civil tiltrotor configurations
By Franklin D. Harris
“Performance analysis of two early NACA high speed propellers with application to civil tiltrotor configurations” Metadata:
- Title: ➤ Performance analysis of two early NACA high speed propellers with application to civil tiltrotor configurations
- Author: Franklin D. Harris
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Performance analysis of two early NACA high speed propellers with application to civil tiltrotor configurations” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Flight envelopes - Reynolds number - Commercial airport - Rotor speed - Rotary wing aircraft - Propeller efficiency - Aircraft design - Tilt rotor aircraft - Tip speed
Edition Identifiers:
- The Open Library ID: OL17837018M - OL15504885M
- Online Computer Library Center (OCLC) ID: 39948229
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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34Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds
By Jack Nugent
“Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds” Metadata:
- Title: ➤ Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds
- Author: Jack Nugent
- Language: English
- Number of Pages: Median: 120
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - Ames Research Center - For sale by the National Technical Information Service]
- Publish Date: 1987 - 1988
- Publish Location: ➤ Edwards, Calif - [Springfield, Va - [Washington, DC]
“Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds” Subjects and Themes:
- Subjects: Aerodynamics, Transonic - Afterbodies - Nozzle flow - Reynolds number - Transonic Aerodynamics
Edition Identifiers:
- The Open Library ID: OL14662959M - OL18998718M
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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35Wing pressure distributions from subsonic tests of a high-wing transport model
By Zachary T. Applin
“Wing pressure distributions from subsonic tests of a high-wing transport model” Metadata:
- Title: ➤ Wing pressure distributions from subsonic tests of a high-wing transport 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
“Wing pressure distributions from subsonic tests of a high-wing transport model” Subjects and Themes:
- Subjects: ➤ Angle of attack - Leading edge flaps - Mach number - Pressure distribution - Reynolds number - Sideslip - Subsonic flow - Trailing edge flaps - Transport aircraft - Wind tunnel tests - Wings
Edition Identifiers:
- The Open Library ID: OL17788775M - OL15411003M
- Online Computer Library Center (OCLC) ID: 32865600
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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36Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results
By Jim A. Penland
“Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results” Metadata:
- Title: ➤ Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results
- Author: Jim A. Penland
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: Hampton, Va - Springfield, VA
“Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Turbulent boundary layer - Aerodynamic coefficients - Body-wing configurations - Reynolds number - Hypersonic forces - Hypersonic boundary layer - Aerodynamic drag - Hypersonic shock - Mach number
Edition Identifiers:
- The Open Library ID: OL17591848M - OL15548849M
- Online Computer Library Center (OCLC) ID: 42677545
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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37Flight Mechanics/Estimation Theory Symposium, 1989
By Flight Mechanics/Estimation Theory Symposium (1989 Goddard Space Flight Center)
“Flight Mechanics/Estimation Theory Symposium, 1989” Metadata:
- Title: ➤ Flight Mechanics/Estimation Theory Symposium, 1989
- Author: ➤ Flight Mechanics/Estimation Theory Symposium (1989 Goddard Space Flight Center)
- Language: English
- Number of Pages: Median: 476
- Publisher: ➤ For sale by the National Technical Information Service, distributor - NASA, Office of Management, Scientific and Technical Information Division - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
- Publish Date: 1989
- Publish Location: ➤ [Washington, DC] - Washington, D.C.] - [Springfield, Va
“Flight Mechanics/Estimation Theory Symposium, 1989” Subjects and Themes:
- Subjects: Reynolds number - Aerofoils
Edition Identifiers:
- The Open Library ID: OL15397983M - OL52888271M
- Online Computer Library Center (OCLC) ID: 223713858
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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38Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
By William G. Johnson
“Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel” Metadata:
- Title: ➤ Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
- Author: William G. Johnson
- 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: ➤ [Springfield, Va - [Washington, D.C.]
“Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel” Subjects and Themes:
- Subjects: ➤ Aerodynamics, Transonic - Aerofoils - Airfoil profiles - Boeing aircraft - Cryogenic wind tunnels - High Reynolds number - Pressure distribution - Reynolds number - Statistics - Supercritical airfoils - Testing - Transonic Aerodynamics - Two dimensional bodies - Wind tunnel models - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17727212M - OL17634944M
- Online Computer Library Center (OCLC) ID: 166902755
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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39Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing
By Sheryll Goecke Powers
“Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing” Metadata:
- Title: ➤ Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing
- Author: Sheryll Goecke Powers
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - National Technical Information Service, distributor]
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing” Subjects and Themes:
- Subjects: ➤ Boundary layers - Flight tests - Pressure distribution - Pressure measurement - Swept wings - Angle of attack - Reynolds number - Mach number - Supercritical wings
Edition Identifiers:
- The Open Library ID: OL17839404M - OL15548584M
- Online Computer Library Center (OCLC) ID: 41964681
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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40Drag reduction on circular cylinders by ejecting jet from rear stagnation region
By S. Atsuchi
“Drag reduction on circular cylinders by ejecting jet from rear stagnation region” Metadata:
- Title: ➤ Drag reduction on circular cylinders by ejecting jet from rear stagnation region
- Author: S. Atsuchi
- Language: English
- Publisher: ➤ Dept. of Mechanical Engineering, College of Engineering and Technology, Old Dominion University - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC - Norfolk, Va
“Drag reduction on circular cylinders by ejecting jet from rear stagnation region” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Drag reduction - Reynolds number - Pressure measurement - Stagnation point - Ejection - Finite volume method - Navier-Stokes equation - Circular cylinders - Algorithms - Injection
Edition Identifiers:
- The Open Library ID: OL17826956M - OL15491664M
- Online Computer Library Center (OCLC) ID: 39097177
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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41Water-tunnel study of transition flow around circular cylinders
By D Almosnino
“Water-tunnel study of transition flow around circular cylinders” Metadata:
- Title: ➤ Water-tunnel study of transition flow around circular cylinders
- Author: D Almosnino
- Language: English
- Number of Pages: Median: 31
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1984
- Publish Location: ➤ [Springfield, Va - Washington, D.C
“Water-tunnel study of transition flow around circular cylinders” Subjects and Themes:
- Subjects: Reynolds number
Edition Identifiers:
- The Open Library ID: OL16806773M - OL17977462M
Access and General Info:
- First Year Published: 1984
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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42Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel
By Theodore R. Creel
“Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel” Metadata:
- Title: ➤ Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel
- Author: Theodore R. Creel
- 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: ➤ [Springfield, Va - [Washington, D.C.]
“Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel” Subjects and Themes:
- Subjects: Reynolds number - Supersonic wind tunnels - Boundary layer noise
Edition Identifiers:
- The Open Library ID: OL17673122M - OL17835443M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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43Computations of complex three-dimensional turbulent free jets
By Robert V. Wilson
“Computations of complex three-dimensional turbulent free jets” Metadata:
- Title: ➤ Computations of complex three-dimensional turbulent free jets
- Author: Robert V. Wilson
- Language: English
- Publisher: ➤ Institute for Computational and Applied Mechanics, Old Dominion University - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Norfolk, Va - [Washington, DC - Springfield, Va
“Computations of complex three-dimensional turbulent free jets” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Poisson equation - Reynolds number - Three dimensional flow - Finite difference theory - Navier-Stokes equation - Turbulent jets - Free jets - Incompressible flow - Runge-Kutta method
Edition Identifiers:
- The Open Library ID: OL17837876M - OL15538163M
- Online Computer Library Center (OCLC) ID: 40556376
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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44Effects of large-scale intermittency of turbulence on scalar spectra at high wave numbers
By Reginald J. Hill
“Effects of large-scale intermittency of turbulence on scalar spectra at high wave numbers” Metadata:
- Title: ➤ Effects of large-scale intermittency of turbulence on scalar spectra at high wave numbers
- Author: Reginald J. Hill
- Language: English
- Number of Pages: Median: 19
- Publisher: ➤ U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories
- Publish Date: 1980
- Publish Location: Boulder, Colo
“Effects of large-scale intermittency of turbulence on scalar spectra at high wave numbers” Subjects and Themes:
- Subjects: Scalar field theory - Reynolds number - Atmospheric turbulence
Edition Identifiers:
- The Open Library ID: OL17956310M - OL13604409M
Access and General Info:
- First Year Published: 1980
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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45Aerothermodynamic calculations on X-34 at Mach 6 wind tunnel conditions
By William A. Wood
“Aerothermodynamic calculations on X-34 at Mach 6 wind tunnel conditions” Metadata:
- Title: ➤ Aerothermodynamic calculations on X-34 at Mach 6 wind tunnel conditions
- Author: William A. Wood
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1999
- Publish Location: Hampton, Va - [Springfield, Va
“Aerothermodynamic calculations on X-34 at Mach 6 wind tunnel conditions” Subjects and Themes:
- Subjects: ➤ Aerodynamic heating - Aerothermodynamics - Baldwin-Lomax turbulence model - Hypersonic heat transfer - Laminar boundary layer - Reynolds number - Turbulence effects - Turbulent boundary layer - Wind tunnel tests - X-34 reusable launch vehicle
Edition Identifiers:
- The Open Library ID: OL17839053M - OL15542540M
- Online Computer Library Center (OCLC) ID: 41469786
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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46Viscous flow in a rectangular cut-out
By Zeev Rotem
“Viscous flow in a rectangular cut-out” Metadata:
- Title: ➤ Viscous flow in a rectangular cut-out
- Author: Zeev Rotem
- Language: English
- Number of Pages: Median: 39
- Publisher: ➤ Dept. of Mechanical Engineering, Faculty of Applied Science, University of British Columbia
- Publish Date: 1965
- Publish Location: [Vancouver]
“Viscous flow in a rectangular cut-out” Subjects and Themes:
- Subjects: Fluid dynamics - Piezometer - Reynolds number
Edition Identifiers:
- The Open Library ID: OL4586644M
- Library of Congress Control Number (LCCN): 77244608
Access and General Info:
- First Year Published: 1965
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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47Evaluation of high reynolds number flow in a 180 degree turn-around duct
By Virgil A. Sandborn
“Evaluation of high reynolds number flow in a 180 degree turn-around duct” Metadata:
- Title: ➤ Evaluation of high reynolds number flow in a 180 degree turn-around duct
- Author: Virgil A. Sandborn
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1991
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Evaluation of high reynolds number flow in a 180 degree turn-around duct” Subjects and Themes:
- Subjects: Reynolds number
Edition Identifiers:
- The Open Library ID: OL15370115M
Author's Alternative Names:
"Virgil A Sandborn"Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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48Flow distribution around the SSME main injector assembly using porosity formulation
By Gary C. Cheng
“Flow distribution around the SSME main injector assembly using porosity formulation” Metadata:
- Title: ➤ Flow distribution around the SSME main injector assembly using porosity formulation
- Author: Gary C. Cheng
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Flow distribution around the SSME main injector assembly using porosity formulation” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Drag - Flow distribution - Gas flow - High temperature gases - Injectors - Navier-Stokes equation - Porosity - Reynolds number - Space shuttle main engine - Turbulent flow
Edition Identifiers:
- The Open Library ID: OL15506214M
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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49Experimental measurements of sonic boom signatures using a continuous data acquistion technique
By Floyd J. Wilcox
“Experimental measurements of sonic boom signatures using a continuous data acquistion technique” Metadata:
- Title: ➤ Experimental measurements of sonic boom signatures using a continuous data acquistion technique
- Author: Floyd J. Wilcox
- Language: English
- Number of Pages: Median: 45
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 2013
- Publish Location: Hampton, Virginia
“Experimental measurements of sonic boom signatures using a continuous data acquistion technique” Subjects and Themes:
- Subjects: ➤ Angle of attack - Data acquisition - Information flow - Mach number - Reynolds number - Sonic booms - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL43222315M
- Online Computer Library Center (OCLC) ID: 880928070
Access and General Info:
- First Year Published: 2013
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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50Effects of large-scale intermittency of turbulence on scalar spectra at high wave numbers
By Reginald J. Hill
“Effects of large-scale intermittency of turbulence on scalar spectra at high wave numbers” Metadata:
- Title: ➤ Effects of large-scale intermittency of turbulence on scalar spectra at high wave numbers
- Author: Reginald J. Hill
- Language: English
- Number of Pages: Median: 19
- Publisher: ➤ U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories
- Publish Date: 1980
- Publish Location: Boulder, Colo
“Effects of large-scale intermittency of turbulence on scalar spectra at high wave numbers” Subjects and Themes:
- Subjects: Scalar field theory - Reynolds number - Atmospheric turbulence
Edition Identifiers:
- The Open Library ID: OL15252729M - OL22432178M - OL17544798M - OL18020956M - OL17072088M
- Online Computer Library Center (OCLC) ID: 7030386
Access and General Info:
- First Year Published: 1980
- Is Full Text Available: Yes
- Is The Book Public: Yes
- Access Status: Public
Online Access
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- Borrowing from Open Library: Borrowing link
- Borrowing from Archive.org: Borrowing link
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