Explore: Low Speed
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Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1NASA low-speed axial compressor for fundamental research
By Charles A. Wasserbauer
“NASA low-speed axial compressor for fundamental research” Metadata:
- Title: ➤ NASA low-speed axial compressor for fundamental research
- Author: Charles A. Wasserbauer
- Language: English
- Number of Pages: Median: 11
- Publisher: ➤ Lewis Research Center - National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1995
- Publish Location: ➤ Cleveland, Ohio - [Washington, D.C.] - [Springfield, Va - [Washington, DC]
“NASA low-speed axial compressor for fundamental research” Subjects and Themes:
- Subjects: ➤ Turbocompressors - Test facilities - Hubs - Cases (Containers) - Internal flow - Low speed - Compressor blades
Edition Identifiers:
- The Open Library ID: ➤ OL19001848M - OL15417892M - OL18079904M - OL17012100M - OL18083441M - OL15411404M - OL17115000M - OL16984621M
- Online Computer Library Center (OCLC) ID: 33957706 - 32889675
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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2Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept
By David E. Hahne
“Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept” Metadata:
- Title: ➤ Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept
- Author: David E. Hahne
- Language: English
- Number of Pages: Median: 23
- Publisher: ➤ Available from the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - Springfield, VA - Hampton, Va
“Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Aerodynamic coefficients - Aerodynamic stability - Aerodynamics, Hypersonic - Angle of attack - Hypersonic Aerodynamics - Hypersonic speed - Hypersonic vehicles - Low speed - Mach number - Pitching moments - Stability - Stability of airplanes - Stabilizers (Fluid dynamics) - Vortices - Waveriders - Wind tunnel stability tests
Edition Identifiers:
- The Open Library ID: OL18134999M - OL17133262M - OL17839424M - OL21033491M - OL15549003M
- Online Computer Library Center (OCLC) ID: 42055832
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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3Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊
By Scott P. Fears
“Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊” Metadata:
- Title: ➤ Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊
- Author: Scott P. Fears
- Language: English
- Number of Pages: Median: 145
- Publisher: ➤ National Aeronautics and Space Administration - Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Hampton, Va - [Washington, DC - Springfield, Va
“Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊” Subjects and Themes:
- Subjects: ➤ Trailing edge flaps - Aspect ratio - Flight stability tests - Stabilizers (Fluid dynamics) - Wind tunnel tests - Wing profiles - Aerodynamic stability - Angle of attack - Stability - Flight control - Low speed - Planforms - Arrow wings - Tail assemblies - Leading edge flaps
Edition Identifiers:
- The Open Library ID: OL19003591M - OL15416719M - OL18082907M - OL17032232M
- Online Computer Library Center (OCLC) ID: 34127880
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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4Control of low-speed turbulent separated flow over a backward-facing ramp
By John C. Lin
“Control of low-speed turbulent separated flow over a backward-facing ramp” Metadata:
- Title: ➤ Control of low-speed turbulent separated flow over a backward-facing ramp
- Author: John C. Lin
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Control of low-speed turbulent separated flow over a backward-facing ramp” Subjects and Themes:
- Subjects: ➤ Turbulent flow - Separated flow - Boundary layer separation - Vortices - Flow characteristics - Vortex generators - Horseshoe vortices - Vortex shedding - Low speed - Angle of attack - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL18075631M - OL15402173M - OL17000678M - OL17113743M
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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5Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system
By Daniel W. Banks
“Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system” Metadata:
- Title: ➤ Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system
- Author: Daniel W. Banks
- Language: English
- Number of Pages: Median: 112
- Publisher: ➤ Langley Research Center - National Technical Information Service, distributor] - National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1987
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, DC]
“Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system” Subjects and Themes:
- Subjects: Trailing edge flaps - Canard configurations - Spanwise blowing - Low speed - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL20986801M - OL18080186M - OL17683879M - OL17115110M
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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6Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70 ̊
By Holly M. Ross
“Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70 ̊” Metadata:
- Title: ➤ Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70 ̊
- Author: Holly M. Ross
- Language: English
- Number of Pages: Median: 140
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - Available from the National Technical Information Service
- Publish Date: 1995
- Publish Location: ➤ Springfield, VA - Hampton, Va - [Springfield, VA
“Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70 ̊” Subjects and Themes:
- Subjects: ➤ Low aspect ratio wings - Radar cross sections - Wind tunnel tests - Dynamic characteristics - Angle of attack - Tailless aircraft - Sideslip - Low speed - Arrow wings - Airplanes - Wings - Stability of airplanes
Edition Identifiers:
- The Open Library ID: OL19146780M - OL17725194M - OL18227631M - OL17141247M
- Online Computer Library Center (OCLC) ID: 33115440
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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7Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets
By Charles J. Trefny
“Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets” Metadata:
- Title: ➤ Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets
- Author: Charles J. Trefny
- Language: English
- Number of Pages: Median: 60
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Branch - Lewis Research Center
- Publish Date: 1986
- Publish Location: ➤ [Washington, D.C.] - Springfield, Va - Cleveland, Ohio
“Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets” Subjects and Themes:
- Subjects: ➤ Supersonic inlets - Supersonic aircraft - Internal compression inlets - Air intakes - Aerodynamics - Low speed - Jet engines
Edition Identifiers:
- The Open Library ID: OL18218668M - OL19985907M - OL16116660M
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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8Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil
By David E. Hahne
“Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil” Metadata:
- Title: ➤ Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil
- Author: David E. Hahne
- Language: English
- Number of Pages: Median: 48
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - Langley Research Center
- Publish Date: 1991
- Publish Location: ➤ [Washington, D.C.] - Springfield, Va - Hampton, Va
“Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil” Subjects and Themes:
- Subjects: ➤ Laminar flow airfoils - Testing - Jet aircraft - Wind tunnel tests - Airplanes - Full scale tests - Flapping - Airfoil profiles - Laminar flow - Low speed - Semispan models - Wings - Aerofoils
Edition Identifiers:
- The Open Library ID: OL18257128M - OL21499524M - OL16135229M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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9Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes
By Gregory M. Catlin
“Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes” Metadata:
- Title: ➤ Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes
- Author: Gregory M. Catlin
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: [Springfield, Va - Hampton, Va
“Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Angle of attack - Flow visualization - Forebodies - Highly maneuverable aircraft - Lift - Low aspect ratio wings - Low speed - Pitching moments - Swept wings - Wind tunnel tests - Wing planforms
Edition Identifiers:
- The Open Library ID: OL17041056M - OL15426200M - OL18088687M
- Online Computer Library Center (OCLC) ID: 35587781
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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10Effects of leading-edge devices on the low-speed aerodynamic characteristics of a highly-swept arrow-wing
By Samuel J. Scott
“Effects of leading-edge devices on the low-speed aerodynamic characteristics of a highly-swept arrow-wing” Metadata:
- Title: ➤ Effects of leading-edge devices on the low-speed aerodynamic characteristics of a highly-swept arrow-wing
- Author: Samuel J. Scott
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1985
- Publish Location: Hampton, Va
“Effects of leading-edge devices on the low-speed aerodynamic characteristics of a highly-swept arrow-wing” Subjects and Themes:
- Subjects: ➤ Airplanes - Leading edge slats - Leading edges (Aerodynamics) - Low speed - Supersonic transports - Swept wings - Wind tunnel tests - Wings, Swept-back
Edition Identifiers:
- The Open Library ID: OL18293366M - OL16154853M
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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11Low speed analysis of mission adaptive flaps on a high speed civil transport configuration
By Victor R. Lessard
“Low speed analysis of mission adaptive flaps on a high speed civil transport configuration” Metadata:
- Title: ➤ Low speed analysis of mission adaptive flaps on a high speed civil transport configuration
- Author: Victor R. Lessard
- 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
“Low speed analysis of mission adaptive flaps on a high speed civil transport configuration” Subjects and Themes:
- Subjects: ➤ Baldwin-Lomax turbulence model - Boundary layer separation - Flapping - Leading edge flaps - Low speed - Mathematical models - Pitching moments - Thin films - Turbulence models
Edition Identifiers:
- The Open Library ID: OL15567867M - OL17595195M
- Online Computer Library Center (OCLC) ID: 44114595
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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12Preconditioning methods for low-speed flows
By E. Turkel
“Preconditioning methods for low-speed flows” Metadata:
- Title: ➤ Preconditioning methods for low-speed flows
- Author: E. Turkel
- Language: English
- Publisher: ➤ Institute for Computer Applications in Science and Engineering, NASA Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: [Springfield, Va - Hampton, VA
“Preconditioning methods for low-speed flows” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Viscous flow - Three dimensional flow - Acoustic velocity - Navier-Stokes equation - Compressible fluids - Compressible flow - Steady state - Low speed - Incompressible flow
Edition Identifiers:
- The Open Library ID: OL15487201M - OL17834296M
- Online Computer Library Center (OCLC) ID: 39009355
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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13A prediction of 3-D viscous flow and performance of the NASA low-speed centrifugal compressor
By John Moore
“A prediction of 3-D viscous flow and performance of the NASA low-speed centrifugal compressor” Metadata:
- Title: ➤ A prediction of 3-D viscous flow and performance of the NASA low-speed centrifugal compressor
- Author: John Moore
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Mechanical Engineering Dept., Virginia Polytechnic Institute and State University
- Publish Date: 1989
- Publish Location: ➤ Blacksburg, Va - [Washington, DC - Springfield, Va
“A prediction of 3-D viscous flow and performance of the NASA low-speed centrifugal compressor” Subjects and Themes:
- Subjects: ➤ Compressors - Impellers - Low speed - Predictions - Three dimensional flow - Turbulent flow
Edition Identifiers:
- The Open Library ID: OL17683405M - OL18078423M
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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14Response of composite materials to low velocity impact
By Srinivasan, K.
“Response of composite materials to low velocity impact” Metadata:
- Title: ➤ Response of composite materials to low velocity impact
- Author: Srinivasan, K.
- Language: English
- Publisher: ➤ US Army Aviation Systems Command, Aviation R&T Activity - National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1991
- Publish Location: ➤ [Springfield, Va - Hampton, Va - [St. Louis, Mo.]
“Response of composite materials to low velocity impact” Subjects and Themes:
- Subjects: ➤ Epoxy resins - Impact tolerances - Impact damage - Impact tests - Polymer matrix composites - Laminates - Low speed - Thermoplastic resins
Edition Identifiers:
- The Open Library ID: OL15405319M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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15Effects of stator indexing on performance in a low speed multistage axial compressor
By Wendy S. Barankiewicz
“Effects of stator indexing on performance in a low speed multistage axial compressor” Metadata:
- Title: ➤ Effects of stator indexing on performance in a low speed multistage axial compressor
- Author: Wendy S. Barankiewicz
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Effects of stator indexing on performance in a low speed multistage axial compressor” Subjects and Themes:
- Subjects: Low speed - Stators - Losses - Turbocompressors - Stator blades
Edition Identifiers:
- The Open Library ID: OL15498502M
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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16NACA 0015 wing pressure and trailing vortex measurements
By Kenneth W. McAlister
“NACA 0015 wing pressure and trailing vortex measurements” Metadata:
- Title: ➤ NACA 0015 wing pressure and trailing vortex measurements
- Author: Kenneth W. McAlister
- Language: English
- Publisher: ➤ National Technical Information Service , distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1991
- Publish Location: ➤ [Springfield, Va - Washington, D.C
“NACA 0015 wing pressure and trailing vortex measurements” Subjects and Themes:
- Subjects: ➤ Vortices - Pressure measurement - Wing tips - Velocity measurement - Trailing edges - Low speed - Semispan models - Wings
Edition Identifiers:
- The Open Library ID: OL17725370M
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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17Numerical speed of sound and its application to schemes for all speeds
By Meng-Sing Liou
“Numerical speed of sound and its application to schemes for all speeds” Metadata:
- Title: ➤ Numerical speed of sound and its application to schemes for all speeds
- Author: Meng-Sing Liou
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 1999
- Publish Location: ➤ [Cleveland, Ohio] - [Springfield, Va
“Numerical speed of sound and its application to schemes for all speeds” Subjects and Themes:
- Subjects: ➤ Inviscid flow - Turbulent flow - High speed - Ideal gas - Low speed - Acoustic velocity - Multiphase flow
Edition Identifiers:
- The Open Library ID: OL15557207M
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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18A 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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19Numerical speed of sound and its application to schemes for all speeds
By M. S. Liou
“Numerical speed of sound and its application to schemes for all speeds” Metadata:
- Title: ➤ Numerical speed of sound and its application to schemes for all speeds
- Author: M. S. Liou
- 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
“Numerical speed of sound and its application to schemes for all speeds” Subjects and Themes:
- Subjects: ➤ Inviscid flow - Turbulent flow - High speed - Ideal gas - Low speed - Acoustic velocity - Multiphase flow
Edition Identifiers:
- The Open Library ID: OL17136288M
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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20Effect of speed (centrifugal load) on gear crack propagation direction
By David G. Lewicki
“Effect of speed (centrifugal load) on gear crack propagation direction” Metadata:
- Title: ➤ Effect of speed (centrifugal load) on gear crack propagation direction
- Author: David G. Lewicki
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - Available from NASA Center for Aerospace Information
- Publish Date: 2001
- Publish Location: ➤ [Cleveland, Ohio] - Hanover, MD
“Effect of speed (centrifugal load) on gear crack propagation direction” Subjects and Themes:
- Subjects: Crack propagation - Low speed - Gears - Centrifugal force - Transition points
Edition Identifiers:
- The Open Library ID: OL16035840M
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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21Summary of a study to determine low-velocity impact damage and residual tension strength for a thick graphite/epoxy motor case
By C. C. Poe
“Summary of a study to determine low-velocity impact damage and residual tension strength for a thick graphite/epoxy motor case” Metadata:
- Title: ➤ Summary of a study to determine low-velocity impact damage and residual tension strength for a thick graphite/epoxy motor case
- Author: C. C. Poe
- Language: English
- Number of Pages: Median: 34
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1990
- Publish Location: Hampton, Va
“Summary of a study to determine low-velocity impact damage and residual tension strength for a thick graphite/epoxy motor case” Subjects and Themes:
- Subjects: ➤ Propulsion systems - Critical pressure - Space shuttles - Impact damage - Graphite-epoxy composites - Materials - Impact testing - Residual strength - Low speed - Rocket engine cases
Edition Identifiers:
- The Open Library ID: OL16122059M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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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22Planetary and primitive object strength measurements and sampling apparatus
By T. J. Ahrens
“Planetary and primitive object strength measurements and sampling apparatus” Metadata:
- Title: ➤ Planetary and primitive object strength measurements and sampling apparatus
- Author: T. J. Ahrens
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - California Institute of Technology, Seismological Laboratory
- Publish Date: 1997
- Publish Location: ➤ Pasadena, Calif - [Washington, DC - Springfield, Va
“Planetary and primitive object strength measurements and sampling apparatus” Subjects and Themes:
- Subjects: ➤ Penetration - Brittle materials - Compressive strength - Low speed - Targets - Momentum
Edition Identifiers:
- The Open Library ID: OL15506802M
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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23Evaluation of the impact response of textile composites
By M. A. Portanova
“Evaluation of the impact response of textile composites” Metadata:
- Title: ➤ Evaluation of the impact response of textile composites
- Author: M. A. Portanova
- 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
“Evaluation of the impact response of textile composites” Subjects and Themes:
- Subjects: ➤ Braided composites - Impact tolerances - Impact resistance - Sewing - Impact damage - Impact tests - Woven composites - Laminates - Low speed - Textiles
Edition Identifiers:
- The Open Library ID: OL18087866M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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24A comparison of quasi-static indentation to low-velocity impact
By A. T. Nettles
“A comparison of quasi-static indentation to low-velocity impact” Metadata:
- Title: ➤ A comparison of quasi-static indentation to low-velocity impact
- Author: A. T. Nettles
- Language: English
- Number of Pages: Median: 83
- Publisher: ➤ National Aeronautics and Space Administration, Marshall Space Flight Center
- Publish Date: 2000
- Publish Location: MSFC, AL
“A comparison of quasi-static indentation to low-velocity impact” Subjects and Themes:
- Subjects: ➤ Impact testing - Composite materials - Metals - Low speed - Impact tests - Indentation - Static tests - Mechanical properties
Edition Identifiers:
- The Open Library ID: OL17621344M
- Online Computer Library Center (OCLC) ID: 703646099 - 55626818
Access and General Info:
- First Year Published: 2000
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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