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Source: The Open Library
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Search results from The Open Library
1Numerical simulation of the SOFIA flowfield
By Stephen P. Klotz
“Numerical simulation of the SOFIA flowfield” Metadata:
- Title: ➤ Numerical simulation of the SOFIA flowfield
- Author: Stephen P. Klotz
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - MCAT Institute - National Aeronautics and Space Administration
- Publish Date: 1994 - 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC - San Jose, CA
“Numerical simulation of the SOFIA flowfield” Subjects and Themes:
- Subjects: ➤ Active control - Aerodynamic stalling - Airfoils - Boeing 747 aircraft - Boundary layer control - Cavities - Flow distribution - Leading edges - SOFIA (Airborne observatory) - Separated flow - Sound pressure - Tail assemblies - Telescopes - Unsteady flow - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17788523M - OL17791647M - OL18081185M - OL18078541M - OL17683431M
- Online Computer Library Center (OCLC) ID: 33433883 - 32647393
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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2Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements
By W. Lance Richards
“Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements” Metadata:
- Title: ➤ Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements
- Author: W. Lance Richards
- Language: English
- Number of Pages: Median: 14
- Publisher: ➤ Available from the NASA Center for AeroSpace Information] - National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - [Linthicum Heights, MD - [Washington, D.C.]
“Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Aerodynamics, Hypersonic - Boundary layer transition - Data processing - Design and construction - Finite element method - Hypersonic Aerodynamics - Hypersonic planes - Hypersonic speed - Leading edges - Research - Structural design
Edition Identifiers:
- The Open Library ID: OL18134772M - OL19433479M - OL15548269M - OL17132909M - OL17839410M
- Online Computer Library Center (OCLC) ID: 41975259
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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3High-lift systems on commercial subsonic airliners
By Peter K. C. Rudolph
“High-lift systems on commercial subsonic airliners” Metadata:
- Title: ➤ High-lift systems on commercial subsonic airliners
- Author: Peter K. C. Rudolph
- Language: English
- Number of Pages: Median: 155
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“High-lift systems on commercial subsonic airliners” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Aeronautics, Commercial - Airplanes - Attitude (Inclination) - Commercial Aeronautics - Commercial aircraft - Cost analysis - Design analysis - Design and construction - Leading edge flaps - Leading edges - Lift (Aerodynamics) - Lift devices - Trailing edge flaps - Trailing edges - Wing camber - Wing loading - Wing slots
Edition Identifiers:
- The Open Library ID: OL15504955M - OL17576368M - OL18121439M - OL17125763M - OL19287956M
- Online Computer Library Center (OCLC) ID: 39916172
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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4Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate)
By M. N. Kogan
“Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate)” Metadata:
- Title: ➤ Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate)
- Author: M. N. Kogan
- Language: English
- Number of Pages: Median: 44
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center - Available from NASA Center for AeroSpace Information
- Publish Date: 1997
- Publish Location: ➤ Linthicum Heights, MD - [Springfield, Va - Hampton, Va
“Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate)” Subjects and Themes:
- Subjects: ➤ Amplification - Boundary layer - Boundary layer flow - Boundary layer transition - Boundary layers - Flow distortion - Free flow - Inhomogeneity - Laminar flow - Leading edges - Nonuniformity - Reynolds number - Vortex-motion - Wakes - Wire
Edition Identifiers:
- The Open Library ID: OL20887494M - OL18122412M - OL15508905M - OL17574799M - OL17126862M
- Online Computer Library Center (OCLC) ID: 40341327
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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5Finite element elastic-plastic-creep and cyclic life analysis of a cowl lip
By V. K. Arya
“Finite element elastic-plastic-creep and cyclic life analysis of a cowl lip” Metadata:
- Title: ➤ Finite element elastic-plastic-creep and cyclic life analysis of a cowl lip
- Author: V. K. Arya
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration
- Publish Date: 1990
- Publish Location: [Washington, D.C.]
“Finite element elastic-plastic-creep and cyclic life analysis of a cowl lip” Subjects and Themes:
- Subjects: ➤ Finite element method - Strain distribution - Stress distribution - Engine inlets - Life (Durability) - Leading edges - Stress concentration
Edition Identifiers:
- The Open Library ID: OL20571067M - OL17630361M - OL18250118M - OL17725732M
- Online Computer Library Center (OCLC) ID: 62869280
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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6Low-speed aerodynamic data for an 0.18-scale model of an F-16XL with various leading-edge modifications
By David E. Hahne
“Low-speed aerodynamic data for an 0.18-scale model of an F-16XL with various leading-edge modifications” Metadata:
- Title: ➤ Low-speed aerodynamic data for an 0.18-scale model of an F-16XL with various leading-edge modifications
- Author: David E. Hahne
- Language: English
- Publisher: ➤ National Technical Information Service [distributor - Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1999
- Publish Location: ➤ Hanover, MD - Springfield, VA - Hampton, Va
“Low-speed aerodynamic data for an 0.18-scale model of an F-16XL with various leading-edge modifications” Subjects and Themes:
- Subjects: Databases - Leading edges - Scale models
Edition Identifiers:
- The Open Library ID: OL17594999M - OL15568015M - OL18139938M - OL18295719M
- Online Computer Library Center (OCLC) ID: 44121256
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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7A laser-based ice shape profilometer for use in icing wind tunnels
By Edward A. Hovenac
“A laser-based ice shape profilometer for use in icing wind tunnels” Metadata:
- Title: ➤ A laser-based ice shape profilometer for use in icing wind tunnels
- Author: Edward A. Hovenac
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“A laser-based ice shape profilometer for use in icing wind tunnels” Subjects and Themes:
- Subjects: ➤ Laser applications - Ice formation - Wind tunnel tests - Ice - Shapes - Airfoils - Lasers - Wind tunnel models - Leading edges - Profilometers - Imaging techniques
Edition Identifiers:
- The Open Library ID: OL18081560M - OL17116376M - OL15414406M - OL17022695M
- Online Computer Library Center (OCLC) ID: 33958974
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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8Finite element thermo-viscoplastic analysis of aerospace structures
By Ajay K. Pandey
“Finite element thermo-viscoplastic analysis of aerospace structures” Metadata:
- Title: ➤ Finite element thermo-viscoplastic analysis of aerospace structures
- Author: Ajay K. Pandey
- Language: English
- Publisher: NASA Langley Research Center
- Publish Date: 1990
- Publish Location: Hampton, Va
“Finite element thermo-viscoplastic analysis of aerospace structures” Subjects and Themes:
- Subjects: ➤ Viscoplasticity - Aircraft structures - Aerodynamic loads - Thermal stresses - Aerodynamic interference - Hypersonic vehicles - Aerothermodynamics - Finite element method - Aerodynamic heating - Leading edges - Thermoelasticity - Plastic deformation - Thermal analysis - Structural analysis
Edition Identifiers:
- The Open Library ID: OL19146742M - OL17725177M - OL17630485M - OL18227548M
- Online Computer Library Center (OCLC) ID: 60361554
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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9F-18 High Alpha Research Vehicle surface pressures
By David F. Fisher
“F-18 High Alpha Research Vehicle surface pressures” Metadata:
- Title: ➤ F-18 High Alpha Research Vehicle surface pressures
- Author: David F. Fisher
- Language: English
- Number of Pages: Median: 36
- Publisher: ➤ National Technical Information Service, distributor] - NASA Ames Resarch Center, Dryden Flight Research Facility
- Publish Date: 1990 - 1991
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“F-18 High Alpha Research Vehicle surface pressures” Subjects and Themes:
- Subjects: ➤ Flow visualization - Aerodynamic load - F-18 aircraft - Pressure distribution - Wind tunnel tests - Forebodies - Angle of attack - Flight tests - Leading edges - Mach number
Edition Identifiers:
- The Open Library ID: OL20571043M - OL18249920M - OL17633879M - OL16132243M
- Online Computer Library Center (OCLC) ID: 57136710
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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10Sensitivity of F-106B leading-edge-vortex images to flight and vapor-screen parameters
By John E. Lamar
“Sensitivity of F-106B leading-edge-vortex images to flight and vapor-screen parameters” Metadata:
- Title: ➤ Sensitivity of F-106B leading-edge-vortex images to flight and vapor-screen parameters
- Author: John E. Lamar
- Language: English
- Number of Pages: Median: 77
- Publisher: ➤ Langley Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service
- Publish Date: 1988
- Publish Location: ➤ [Washington, D.C.] - Hampton, Va - Springfield, Va
“Sensitivity of F-106B leading-edge-vortex images to flight and vapor-screen parameters” Subjects and Themes:
- Subjects: ➤ Vortices - F-106 aircraft - Vapors - Transonic flight - Flow visualization - Leading edges - Screen effect - Image processing - Wings - Fighter aircraft - Image enhancement - Vapor-screen technique
Edition Identifiers:
- The Open Library ID: OL18468575M - OL16115015M - OL18217721M - OL20898829M
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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11Control 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
Online Access
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12SiC/SiC leading edge turbine airfoil tested under simulated gas turbine conditions
By R. Craig Robinson
“SiC/SiC leading edge turbine airfoil tested under simulated gas turbine conditions” Metadata:
- Title: ➤ SiC/SiC leading edge turbine airfoil tested under simulated gas turbine conditions
- Author: R. Craig Robinson
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: ➤ [Cleveland, Ohio] - Springfield, VA
“SiC/SiC leading edge turbine airfoil tested under simulated gas turbine conditions” Subjects and Themes:
- Subjects: Silicon - Leading edges - Gas turbine engines - Airfoils - Design analysis
Edition Identifiers:
- The Open Library ID: OL17137582M - OL17592610M - OL17702889M
- Online Computer Library Center (OCLC) ID: 43474494
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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13Compressible Navier-Stokes equations
By S. I. Hariharan
“Compressible Navier-Stokes equations” Metadata:
- Title: ➤ Compressible Navier-Stokes equations
- Author: S. I. Hariharan
- Language: English
- Number of Pages: Median: 24
- Publisher: ➤ For sale by the National Technical Information Service - ICASE - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1987
- Publish Location: Hampton, Va - [Springfield, Va
“Compressible Navier-Stokes equations” Subjects and Themes:
- Subjects: Leading edges - Navier-Stokes equation - Fluid mechanics - Navier-Stokes equations
Edition Identifiers:
- The Open Library ID: OL15282874M - OL18031389M - OL19248025M
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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14Transonic 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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15The structure of separated flow regions occurring near the leading edge of airfoils, including transition
By T. J. Mueller
“The structure of separated flow regions occurring near the leading edge of airfoils, including transition” Metadata:
- Title: ➤ The structure of separated flow regions occurring near the leading edge of airfoils, including transition
- Author: T. J. Mueller
- Language: English
- Publisher: ➤ National Technical Information Service - National Technical Information Service, distributor - Dept. of Aerospace and Mechanical Engineering, University of Notre Dame - National Aeronautics and Space Administration
- Publish Date: 1985 - 1986
- Publish Location: ➤ Notre Dame, Ind - [Springfield, Va - [Washington, D.C - Springfield, Va
“The structure of separated flow regions occurring near the leading edge of airfoils, including transition” Subjects and Themes:
- Subjects: ➤ Aerofoils - Airfoils - Boundary layer transition - Bubbles - Leading edges - Separated flow - Velocity distribution
Edition Identifiers:
- The Open Library ID: OL15416442M - OL15394429M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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16Numerical studies of boundary-layer receptivity
By Helen L. Reed
“Numerical studies of boundary-layer receptivity” Metadata:
- Title: ➤ Numerical studies of boundary-layer receptivity
- Author: Helen L. Reed
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Numerical studies of boundary-layer receptivity” Subjects and Themes:
- Subjects: ➤ Alternating direction implicit methods - Boundary layer flow - Far fields - Flat plates - Flow velocity - Incompressible flow - Leading edges - Navier-Stokes equation - Time dependence - Tollmien-Schlichting waves
Edition Identifiers:
- The Open Library ID: OL15420536M - OL17793338M
- Online Computer Library Center (OCLC) ID: 34619740
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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173D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
By M. Mizukami
“3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Metadata:
- Title: ➤ 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
- Author: M. Mizukami
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Boundary layers - Supersonic diffusers - Computational grids - Boundary layer separation - Turbulence models - Three dimensional flow - Flow distribution - Engine inlets - Internal flow - Leading edges - Shock wave interaction - Navier-Stokes equation - Shock waves
Edition Identifiers:
- The Open Library ID: OL17117540M - OL17106503M
- Online Computer Library Center (OCLC) ID: 35282961
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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18Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV
By David F. Fisher
“Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV” Metadata:
- Title: ➤ Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV
- Author: David F. Fisher
- Language: English
- Publisher: ➤ National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV” Subjects and Themes:
- Subjects: ➤ F-18 aircraft - Strakes - Pressure distribution - Aerodynamics - Angle of attack - Flow visualization - Leading edges - Yawing moments
Edition Identifiers:
- The Open Library ID: OL15548262M - OL17839408M
- Online Computer Library Center (OCLC) ID: 41975207
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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193D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
By Masashi Mizukami
“3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Metadata:
- Title: ➤ 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
- Author: Masashi Mizukami
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Boundary layers - Supersonic diffusers - Computational grids - Boundary layer separation - Turbulence models - Three dimensional flow - Flow distribution - Engine inlets - Internal flow - Leading edges - Shock wave interaction - Navier-Stokes equation - Shock waves
Edition Identifiers:
- The Open Library ID: OL18086923M - OL15423278M
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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20Lee-side flow over delta wings at supersonic speeds
By David S. Miller
“Lee-side flow over delta wings at supersonic speeds” Metadata:
- Title: ➤ Lee-side flow over delta wings at supersonic speeds
- Author: David S. Miller
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service
- Publish Date: 1985
- Publish Location: ➤ [Washington, D.C.] - Springfield, Va
“Lee-side flow over delta wings at supersonic speeds” Subjects and Themes:
- Subjects: Delta wings - Supersonic speed - Leading edges - Flow visualization - Vortices
Edition Identifiers:
- The Open Library ID: OL18217697M - OL16114989M
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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21Lee-side flow over delta wings at supersonic speeds
By D. S. Miller
“Lee-side flow over delta wings at supersonic speeds” Metadata:
- Title: ➤ Lee-side flow over delta wings at supersonic speeds
- Author: D. S. Miller
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1985
- Publish Location: ➤ [Washington, D.C.] - Springfield, Va
“Lee-side flow over delta wings at supersonic speeds” Subjects and Themes:
- Subjects: Delta wings - Flow visualization - Leading edges - Supersonic speed - Vortices
Edition Identifiers:
- The Open Library ID: OL18468528M
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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22The effects of the critical ice accretion on airfoil and wing performance
By Michael S. Selig
“The effects of the critical ice accretion on airfoil and wing performance” Metadata:
- Title: ➤ The effects of the critical ice accretion on airfoil and wing performance
- Author: Michael S. Selig
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ [Washington, DC - Springfield, Va
“The effects of the critical ice accretion on airfoil and wing performance” Subjects and Themes:
- Subjects: Aerodynamic characteristics - Airfoils - Design analysis - Ice formation - Leading edges
Edition Identifiers:
- The Open Library ID: OL15547339M
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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23Receptivity 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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24Fabrication and testing of a leading-edge-shaped heat pipe
By David E. Glass
“Fabrication and testing of a leading-edge-shaped heat pipe” Metadata:
- Title: ➤ Fabrication and testing of a leading-edge-shaped heat pipe
- Author: David E. Glass
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: [Springfield, Va - Hampton, Va
“Fabrication and testing of a leading-edge-shaped heat pipe” Subjects and Themes:
- Subjects: Leading edges - Heat pipes - Sharp leading edges - Induction heating - Fabrication
Edition Identifiers:
- The Open Library ID: OL17839119M
- Online Computer Library Center (OCLC) ID: 41347644
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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25Leading-edge receptivity for blunt-nose bodies
By P. W. Hammerton
“Leading-edge receptivity for blunt-nose bodies” Metadata:
- Title: ➤ Leading-edge receptivity for blunt-nose bodies
- Author: P. W. Hammerton
- Publisher: ➤ Arizona University, Dept. of Aerospace and Mechanical Engineering
- Publish Date: 1992
- Publish Location: Tucson, Ariz
“Leading-edge receptivity for blunt-nose bodies” Subjects and Themes:
- Subjects: Leading edges - Blunt bodies
Edition Identifiers:
- The Open Library ID: OL20272145M
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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26Flat plate leading edge receptivity to various freestream disturbance structures
By Roland Adolf Eberhard Heinrich
“Flat plate leading edge receptivity to various freestream disturbance structures” Metadata:
- Title: ➤ Flat plate leading edge receptivity to various freestream disturbance structures
- Author: Roland Adolf Eberhard Heinrich
- Number of Pages: Median: 236
- Publisher: University of Arizona
- Publish Date: 1989
- Publish Location: [Tucson, Ariz.]
“Flat plate leading edge receptivity to various freestream disturbance structures” Subjects and Themes:
- Subjects: Leading edges - Receptivity
Edition Identifiers:
- The Open Library ID: OL21334917M
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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27The response of the unsteady laminar boundary layer to leading edge acoustic diffraction
By Steven John Hulshoff
“The response of the unsteady laminar boundary layer to leading edge acoustic diffraction” Metadata:
- Title: ➤ The response of the unsteady laminar boundary layer to leading edge acoustic diffraction
- Author: Steven John Hulshoff
- Number of Pages: Median: 62
- Publisher: ➤ Department of Aerospace Science and Engineering
- Publish Date: 1989
- Publish Location: [Downsview, Ont.]
“The response of the unsteady laminar boundary layer to leading edge acoustic diffraction” Subjects and Themes:
- Subjects: Laminar boundary layer - Acoustic excitation - Leading edges
Edition Identifiers:
- The Open Library ID: OL18929507M
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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28Effect of a rotor wake on the local heat transfer on the forward half of a circular cylinder
By Kim A. Morehouse
“Effect of a rotor wake on the local heat transfer on the forward half of a circular cylinder” Metadata:
- Title: ➤ Effect of a rotor wake on the local heat transfer on the forward half of a circular cylinder
- Author: Kim A. Morehouse
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1986
- Publish Location: [Cleveland, Ohio
“Effect of a rotor wake on the local heat transfer on the forward half of a circular cylinder” Subjects and Themes:
- Subjects: ➤ Leading edges - Circular cylinders - Fluid dynamics - Airfoils - Vortices - Heat transfer coefficients - Turbines
Edition Identifiers:
- The Open Library ID: OL16151199M
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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29Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane
By Dennis O. Allison
“Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane” Metadata:
- Title: ➤ Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane
- Author: Dennis O. Allison
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service (NTIS) [distributor
- Publish Date: 1995
- Publish Location: Springfield, VA - Hampton, Va
“Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane” Subjects and Themes:
- Subjects: ➤ Pressure distribution - Wind tunnel tests - Aircraft models - Subsonic speed - Transonic speed - Maneuverability - Trailing edges - Airfoils - Wing-fuselage stores - Leading edges
Edition Identifiers:
- The Open Library ID: OL15413576M
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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30Transonic and supersonic flow past a 65 degree delta wing with rounded leading edges - analysis of experimental data
By Krishnaswami Yegna Narayan
“Transonic and supersonic flow past a 65 degree delta wing with rounded leading edges - analysis of experimental data” Metadata:
- Title: ➤ Transonic and supersonic flow past a 65 degree delta wing with rounded leading edges - analysis of experimental data
- Author: Krishnaswami Yegna Narayan
- Number of Pages: Median: 64
- Publisher: DFVLR
- Publish Date: 1988
- Publish Location: Koln
“Transonic and supersonic flow past a 65 degree delta wing with rounded leading edges - analysis of experimental data” Subjects and Themes:
- Subjects: Delta wings - Leading edges
Edition Identifiers:
- The Open Library ID: OL18928649M
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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31Flow over a leading edge with distributed roughness
By Jerzy M. Floryan
“Flow over a leading edge with distributed roughness” Metadata:
- Title: ➤ Flow over a leading edge with distributed roughness
- Author: Jerzy M. Floryan
- Number of Pages: Median: 49
- Publisher: DFVLR
- Publish Date: 1988
- Publish Location: Koln
“Flow over a leading edge with distributed roughness” Subjects and Themes:
- Subjects: Leading edges - Roughness - Transition flow - Boundary layer - Surface roughness
Edition Identifiers:
- The Open Library ID: OL18928760M
- Online Computer Library Center (OCLC) ID: 26460009
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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32Research towards the development of a structurally integrated optical fiber sensor system for impact detection in aircraft composite leading edge
By Stephane Dubois
“Research towards the development of a structurally integrated optical fiber sensor system for impact detection in aircraft composite leading edge” Metadata:
- Title: ➤ Research towards the development of a structurally integrated optical fiber sensor system for impact detection in aircraft composite leading edge
- Author: Stephane Dubois
- Publisher: University of Toronto
- Publish Date: 1989
- Publish Location: [Downsview, Ont.]
“Research towards the development of a structurally integrated optical fiber sensor system for impact detection in aircraft composite leading edge” Subjects and Themes:
- Subjects: Composite materials - Optical fibers - Damage detection systems - Delaminating - Leading edges
Edition Identifiers:
- The Open Library ID: OL18931769M
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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33Aerothermal performance constraints for hypervelocity small radius unswept leading edges and nosetips
By Paul Kolodziej
“Aerothermal performance constraints for hypervelocity small radius unswept leading edges and nosetips” Metadata:
- Title: ➤ Aerothermal performance constraints for hypervelocity small radius unswept leading edges and nosetips
- Author: Paul Kolodziej
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Aerothermal performance constraints for hypervelocity small radius unswept leading edges and nosetips” Subjects and Themes:
- Subjects: ➤ Ablation - Heating - Aerothermodynamics - Wave drag - Thermal protection - Leading edges - Nose tips - Ceramics
Edition Identifiers:
- The Open Library ID: OL17128484M
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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34Analysis of the leading edge effects on the boundary layer transition
By P. L. Chow
“Analysis of the leading edge effects on the boundary layer transition” Metadata:
- Title: ➤ Analysis of the leading edge effects on the boundary layer transition
- Author: P. L. Chow
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1990
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Analysis of the leading edge effects on the boundary layer transition” Subjects and Themes:
- Subjects: ➤ Feedback control - Boundary layer transition - Boundary layer control - Aerodynamic heating - Leading edges - Active control - Optimal control - Shear flow
Edition Identifiers:
- The Open Library ID: OL15405512M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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35Leading-edge receptivity for blunt-nose bodies
By Edward J. Kerschen
“Leading-edge receptivity for blunt-nose bodies” Metadata:
- Title: ➤ Leading-edge receptivity for blunt-nose bodies
- Author: Edward J. Kerschen
- Number of Pages: Median: 26
- Publisher: Arizona University
- Publish Date: 1991
- Publish Location: Tucson, Ariz
“Leading-edge receptivity for blunt-nose bodies” Subjects and Themes:
- Subjects: Leading edges - Blunt bodies - Receptivity
Edition Identifiers:
- The Open Library ID: OL19245811M
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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36A survey of Reynolds number and wing geometry effects on lift characteristics in the low speed stall region
By Edward C. Polhamus
“A survey of Reynolds number and wing geometry effects on lift characteristics in the low speed stall region” Metadata:
- Title: ➤ A survey of Reynolds number and wing geometry effects on lift characteristics in the low speed stall region
- Author: Edward C. Polhamus
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service [distributor
- Publish Date: 1996
- Publish Location: Springfield, VA - Hampton, Va
“A survey of Reynolds number and wing geometry effects on lift characteristics in the low speed stall region” Subjects and Themes:
- Subjects: Aerodynamic stalling - Leading edges - Low speed - Swept wings - Wing planforms
Edition Identifiers:
- The Open Library ID: OL15490451M
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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37Computation of separated and unsteady flows with one- and two-equation turbulence models
By J. A. Ekaterinaris
“Computation of separated and unsteady flows with one- and two-equation turbulence models” Metadata:
- Title: ➤ Computation of separated and unsteady flows with one- and two-equation turbulence models
- Author: J. A. Ekaterinaris
- Language: English
- Publisher: ➤ [National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ Springfield, Va - Washington, D.C
“Computation of separated and unsteady flows with one- and two-equation turbulence models” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Eddy viscosity - Upwind schemes (Mathematics) - Unsteady flow - Computerized simulation - Turbulence models - Flow distribution - High Reynolds number - Leading edges - Navier-Stokes equation - Transition flow - Separated flow
Edition Identifiers:
- The Open Library ID: OL15501779M
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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38Flight demonstration of a shock location sensor using constant voltage hot-film anemometry
By Timothy R. Moes
“Flight demonstration of a shock location sensor using constant voltage hot-film anemometry” Metadata:
- Title: ➤ Flight demonstration of a shock location sensor using constant voltage hot-film anemometry
- Author: Timothy R. Moes
- Language: English
- Publisher: ➤ National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1997
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Flight demonstration of a shock location sensor using constant voltage hot-film anemometry” Subjects and Themes:
- Subjects: ➤ F-15 aircraft - Hot-film anemometers - Airfoils - Laminar boundary layer - Leading edges - Pressure sensors - Transonic speed
Edition Identifiers:
- The Open Library ID: OL15504664M
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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39Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges
By Julio Chu
“Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges” Metadata:
- Title: ➤ Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges
- Author: Julio Chu
- 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
“Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges” Subjects and Themes:
- Subjects: ➤ Vortices - Pressure distribution - Wind tunnel tests - Subsonic speed - Slender wings - Reynolds number - Delta wings - Leading edges - Mach number
Edition Identifiers:
- The Open Library ID: OL15504600M
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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40Hypersonic engine leading edge experiments in a high heat flux, supersonic flow environment
By Herbert J. Gladden
“Hypersonic engine leading edge experiments in a high heat flux, supersonic flow environment” Metadata:
- Title: ➤ Hypersonic engine leading edge experiments in a high heat flux, supersonic flow environment
- Author: Herbert J. Gladden
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Hypersonic engine leading edge experiments in a high heat flux, supersonic flow environment” Subjects and Themes:
- Subjects: ➤ Heat flux - Leading edges - Hypersonic heat transfer - Thermal stresses - High temperature environments - Hypersonic flight
Edition Identifiers:
- The Open Library ID: OL15408492M
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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41Unsteady, transonic flow around delta wings undergoing coupled and natural modes response
By Margaret Anne Menzies
“Unsteady, transonic flow around delta wings undergoing coupled and natural modes response” Metadata:
- Title: ➤ Unsteady, transonic flow around delta wings undergoing coupled and natural modes response
- Author: Margaret Anne Menzies
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - Old Dominion University - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - [Norfolk, VA - Washington, D.C
“Unsteady, transonic flow around delta wings undergoing coupled and natural modes response” Subjects and Themes:
- Subjects: ➤ Flow equations - Aerodynamic coefficients - Unsteady flow - Transonic flow - Swept wings - Navier-Stokes equation - Angle of attack - Delta wings - Leading edges - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15508551M
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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42Spatial characteristics of the unsteady differential pressures on 16% F/A-18 vertical tails
By Robert W. Moses
“Spatial characteristics of the unsteady differential pressures on 16% F/A-18 vertical tails” Metadata:
- Title: ➤ Spatial characteristics of the unsteady differential pressures on 16% F/A-18 vertical tails
- Author: Robert W. Moses
- Language: English
- Publisher: ➤ American Institute of Aeronautics and Astronautics - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ Springfield, Va - [Washington, DC - Reston, Va
“Spatial characteristics of the unsteady differential pressures on 16% F/A-18 vertical tails” Subjects and Themes:
- Subjects: ➤ F-18 aircraft - Vortices - Angle of attack - Buffeting - Leading edges - Aerodynamic forces - Turbulent wakes - Aeroelasticity
Edition Identifiers:
- The Open Library ID: OL15509422M
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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43Space shuttle pinhole formation mechanism studies
By Nathan S. Jacobson
“Space shuttle pinhole formation mechanism studies” Metadata:
- Title: ➤ Space shuttle pinhole formation mechanism studies
- Author: Nathan S. Jacobson
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ [Cleveland, Ohio] - [Springfield, Va
“Space shuttle pinhole formation mechanism studies” Subjects and Themes:
- Subjects: ➤ Carbon-carbon composites - Leading edges - Microstructure - Pinholes - Space shuttles - Weathering - Wings
Edition Identifiers:
- The Open Library ID: OL15542460M
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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44Lateral shock of the R Aquarii jet
By J. M. Hollis
“Lateral shock of the R Aquarii jet” Metadata:
- Title: ➤ Lateral shock of the R Aquarii jet
- Author: J. M. Hollis
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Lateral shock of the R Aquarii jet” Subjects and Themes:
- Subjects: ➤ Angular momentum - Radio waves - Leading edges - Ultraviolet emission - Stellar mass - Shock waves
Edition Identifiers:
- The Open Library ID: OL15507786M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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45NASA/FAA Tailplane Icing Program
By Thomas P. Ratvasky
“NASA/FAA Tailplane Icing Program” Metadata:
- Title: ➤ NASA/FAA Tailplane Icing Program
- Author: Thomas P. Ratvasky
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2000
- Publish Location: ➤ [Springfield, Va - [Cleveland, Ohio]
“NASA/FAA Tailplane Icing Program” Subjects and Themes:
- Subjects: Aircraft icing - Aircraft stability - Flight tests - Horizontal tail surfaces - Leading edges
Edition Identifiers:
- The Open Library ID: OL15569374M
- Online Computer Library Center (OCLC) ID: 44441990
Access and General Info:
- First Year Published: 2000
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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46Closed form equations for the preliminary design of a heat-pipe-cooled leading edge
By David E. Glass
“Closed form equations for the preliminary design of a heat-pipe-cooled leading edge” Metadata:
- Title: ➤ Closed form equations for the preliminary design of a heat-pipe-cooled leading edge
- Author: David E. Glass
- 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
“Closed form equations for the preliminary design of a heat-pipe-cooled leading edge” Subjects and Themes:
- Subjects: Leading edges - Cooling - Heat pipes - Structural design - Evaluation
Edition Identifiers:
- The Open Library ID: OL15542646M
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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47A simplified method for thermal analysis of a cowl leading edge subject to intense local shock-wave-interference heating
By David M. McGowan
“A simplified method for thermal analysis of a cowl leading edge subject to intense local shock-wave-interference heating” Metadata:
- Title: ➤ A simplified method for thermal analysis of a cowl leading edge subject to intense local shock-wave-interference heating
- Author: David M. McGowan
- Number of Pages: Median: 36
- Publisher: Langley Research Center
- Publish Date: 1992
- Publish Location: Hampton, Va
“A simplified method for thermal analysis of a cowl leading edge subject to intense local shock-wave-interference heating” Subjects and Themes:
- Subjects: Thermal analysis - Shock waves - Cowlings - Leading edges
Edition Identifiers:
- The Open Library ID: OL19243186M
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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48Effects of wing modification on an aircraft's aerodynamic parameters as determined from flight data
By Robert Alan Hess
“Effects of wing modification on an aircraft's aerodynamic parameters as determined from flight data” Metadata:
- Title: ➤ Effects of wing modification on an aircraft's aerodynamic parameters as determined from flight data
- Author: Robert Alan Hess
- Language: English
- Number of Pages: Median: 63
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1986
- Publish Location: Hampton, Va
“Effects of wing modification on an aircraft's aerodynamic parameters as determined from flight data” Subjects and Themes:
- Subjects: ➤ Airplanes - Aerodynamics - Wing profiles - Aircraft stability - Aerodynamic stalling - Leading edges - General aviation aircraft - Wings - Stability of airplanes
Edition Identifiers:
- The Open Library ID: OL16152660M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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49Task 4 supporting technology
By P. A. Hogenson
“Task 4 supporting technology” Metadata:
- Title: Task 4 supporting technology
- Author: P. A. Hogenson
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Rockwell Aerospace, Space Systems Division
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC - [Downey, Calif.] - Springfield, Va
“Task 4 supporting technology” Subjects and Themes:
- Subjects: ➤ Reusable heat shielding - Technology assessment - Thermal insulation - Thermal protection - Reentry shielding - Compression tests - Silicones - Ceramics - Tiles - Ablative materials - Sealers - Aluminum oxides - Leading edges - Coatings - Reusable launch vehicles - High temperature tests
Edition Identifiers:
- The Open Library ID: OL15413910M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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50Boundary layer transition in the leading edge region of a swept cylinder in high speed flow
By Colin P. Coleman
“Boundary layer transition in the leading edge region of a swept cylinder in high speed flow” Metadata:
- Title: ➤ Boundary layer transition in the leading edge region of a swept cylinder in high speed flow
- Author: Colin P. Coleman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ Moffett Field, Calif - Springfield, VA
“Boundary layer transition in the leading edge region of a swept cylinder in high speed flow” Subjects and Themes:
- Subjects: ➤ Boundary layer transition - Reynolds number - Leading edges - Wind tunnel tests - Swept wings - Supersonic flow
Edition Identifiers:
- The Open Library ID: OL15548550M
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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