Explore: *airfoils
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AI-Generated Overview About “%2Bairfoils”:
Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1TADS--a CFD-based turbomachinery analysis and design system with GUI
By M. J. Koiro
“TADS--a CFD-based turbomachinery analysis and design system with GUI” Metadata:
- Title: ➤ TADS--a CFD-based turbomachinery analysis and design system with GUI
- Author: M. J. Koiro
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 1999
- Publish Location: ➤ [Springfield, Va - [Cleveland, Ohio]
“TADS--a CFD-based turbomachinery analysis and design system with GUI” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Turbomachinery - Design analysis - Graphical user interface - User manuals (Computer programs) - Systems analysis - Airfoils - Computer programs
Edition Identifiers:
- The Open Library ID: ➤ OL18136416M - OL17591424M - OL18136413M - OL17591425M - OL17134700M - OL15552394M - OL17134644M
- Online Computer Library Center (OCLC) ID: 42590428 - 42623735
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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2Airfoil self-noise and prediction
By Thomas F. Brooks
“Airfoil self-noise and prediction” Metadata:
- Title: ➤ Airfoil self-noise and prediction
- Author: Thomas F. Brooks
- Language: English
- Number of Pages: Median: 137
- Publisher: ➤ For sale by the National Technical Information Service] - Langley Research Center - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
- Publish Date: 1989
- Publish Location: ➤ [Washington, D.C.] - Washington, D.C - [Springfield, Va - Hampton, Va
“Airfoil self-noise and prediction” Subjects and Themes:
- Subjects: Aerofoils - Aircraft noise - Airfoils - Noise
Edition Identifiers:
- The Open Library ID: ➤ OL18784260M - OL19379562M - OL18028703M - OL15274290M - OL16371202M - OL1812961M
- Library of Congress Control Number (LCCN): 89602569
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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3The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil
By Cuyler W. Brooks
“The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil” Metadata:
- Title: ➤ The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil
- Author: Cuyler W. Brooks
- Language: English
- Number of Pages: Median: 18
- Publisher: ➤ Langley Research Center - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - For sale by the National Technical Information Service
- Publish Date: 1989 - 1991
- Publish Location: ➤ [Washington, D.C.] - Springfield, Va - Hampton, Va
“The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil” Subjects and Themes:
- Subjects: ➤ Aerodynamics, Transonic - Aerofoils - Airfoils - Boundary layer - Boundary layer control - Drag - Drag (Aerodynamics) - Laminar boundary layer - Laminar flow - Laminar flow control - Suction - Supercritical airfoils - Supercritical wings - Swept wings - Testing - Transonic Aerodynamics
Edition Identifiers:
- The Open Library ID: ➤ OL20571034M - OL18930562M - OL17630310M - OL16132232M - OL18249910M - OL20779439M
- Online Computer Library Center (OCLC) ID: 48986179
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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4Free-form airfoil shape optimization under uncertainty using maximum expected value and second-order second-moment strategies
By Luc Huyse
“Free-form airfoil shape optimization under uncertainty using maximum expected value and second-order second-moment strategies” Metadata:
- Title: ➤ Free-form airfoil shape optimization under uncertainty using maximum expected value and second-order second-moment strategies
- Author: Luc Huyse
- Language: English
- Number of Pages: Median: 24
- Publisher: ➤ National Technical Information Service, distributor - ICASE, NASA Langley Research Center - Institute for Computer Applications in Science and Engineering, NASA Langley Research Center - Available from NASA Center for Aerospace Information
- Publish Date: 2001
- Publish Location: ➤ Hampton, VA - Springfield, VA - Hanover, MD
“Free-form airfoil shape optimization under uncertainty using maximum expected value and second-order second-moment strategies” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Aerofoils - Airfoils - Computational fluid dynamics - Control theory - Mathematical models - Mathematical optimization - Shape optimization - Statistical analysis
Edition Identifiers:
- The Open Library ID: OL16031867M - OL18171977M - OL19025798M - OL17607430M - OL18395785M
- Online Computer Library Center (OCLC) ID: 50065898
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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5Numerical 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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6Development of a large-scale, outdoor, ground-based test capability for evaluating the effect of rain on airfoil lift
By Gaudy M. Bezos
“Development of a large-scale, outdoor, ground-based test capability for evaluating the effect of rain on airfoil lift” Metadata:
- Title: ➤ Development of a large-scale, outdoor, ground-based test capability for evaluating the effect of rain on airfoil lift
- Author: Gaudy M. Bezos
- Language: English
- Number of Pages: Median: 65
- Publisher: ➤ National Technical Information Service, distributor] - Langley Research Center - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1993
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, DC]
“Development of a large-scale, outdoor, ground-based test capability for evaluating the effect of rain on airfoil lift” Subjects and Themes:
- Subjects: Lift (Aerodynamics) - Aerofoils - Rain simulation - Airfoils
Edition Identifiers:
- The Open Library ID: OL18062881M - OL17109822M - OL15381995M - OL20272583M - OL14697261M
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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7Numerical solutions of the complete Navier-Stokes equations
By H. A. Hassan
“Numerical solutions of the complete Navier-Stokes equations” Metadata:
- Title: ➤ Numerical solutions of the complete Navier-Stokes equations
- Author: H. A. Hassan
- Language: English
- Publisher: ➤ Dept. of Mechanical and Aerospace Engineering, North Carolina State University - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1989 - 1994 - 1995 - 1996
- Publish Location: ➤ [Washington, DC - [Washington, D.C - Raleigh, N.C - Springfield, Va
“Numerical solutions of the complete Navier-Stokes equations” Subjects and Themes:
- Subjects: ➤ Navier-Stokes equation - Turbulent flow - Turbulence models - Eddy viscosity - Flow velocity - Supersonic combustion - Mixing layers (Fluids) - Jet flow - Navier-Stokes equations - Compressible flow - Compressibility - Numerical solutions - Turbulent mixing - Computational fluid dynamics - Numerical analysis - Vorticity - Boundary layer separation - Vortices - Pressure gradients - Three dimensional flow - Aerodynamic characteristics - Airfoils
Edition Identifiers:
- The Open Library ID: OL15419184M - OL15452379M - OL16135487M - OL14706079M
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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82-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall
By R. A. Piziali
“2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall” Metadata:
- Title: ➤ 2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall
- Author: R. A. Piziali
- Language: English
- Number of Pages: Median: 559
- Publisher: ➤ National Technical Information Service, distributor - Ames Research Center - National Aeronautics and Space Administration, Ames Research Center : US Army Aviation and Troop Command
- Publish Date: 1994
- Publish Location: ➤ Moffett Field, Calif - Moffett Field, Ca - [Springfield, Va
“2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall” Subjects and Themes:
- Subjects: ➤ Rotary wings - Aerodynamic coefficients - Pressure distribution - Wind tunnel tests - Wind oscillations - Angle of attack - Airfoils - Aerodynamic stalling - Semispan models - Stalling - Oscillating wing aerodynamics
Edition Identifiers:
- The Open Library ID: OL17007551M - OL15409387M - OL18079048M - OL19754822M - OL17114716M
- Online Computer Library Center (OCLC) ID: 32770651
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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9The 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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10Assessment of two-equation turbulence models for transonic flows
By Florian R. Menter
“Assessment of two-equation turbulence models for transonic flows” Metadata:
- Title: ➤ Assessment of two-equation turbulence models for transonic flows
- Author: Florian R. Menter
- Language: English
- Publisher: ➤ American Institute of Aeronautics and Astronautics - [National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ Washington, D.C - Springfield, Va
“Assessment of two-equation turbulence models for transonic flows” Subjects and Themes:
- Subjects: ➤ Airfoils - Eddy viscosity - Test chambers - Transonic flow - Wind tunnel walls - Wings
Edition Identifiers:
- The Open Library ID: OL15501783M - OL17593867M - OL17135542M - OL18120478M
- Online Computer Library Center (OCLC) ID: 42787321
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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11A far-field non-reflecting boundary condition for two-dimensional wake flows
By Jeffrey S. Danowitz
“A far-field non-reflecting boundary condition for two-dimensional wake flows” Metadata:
- Title: ➤ A far-field non-reflecting boundary condition for two-dimensional wake flows
- Author: Jeffrey S. Danowitz
- Language: English
- Number of Pages: Median: 32
- Publisher: ➤ Institute for Computer Applications in Science and Engineering, NASA Langley Research Center - Institute for Computer Applications in Science and Engineering - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Hampton, VA - Hampton, Va - [Springfield, Va
“A far-field non-reflecting boundary condition for two-dimensional wake flows” Subjects and Themes:
- Subjects: ➤ Viscous flow - Far fields - Two dimensional flow - Multigrid methods - Numerical analysis - Computational grids - Wakes - Steady flow - Navier-Stokes equation - Grid generation (Mathematics) - Airfoils - Boundary conditions - Compressible flow
Edition Identifiers:
- The Open Library ID: OL19005099M - OL17087873M - OL18085483M - OL15420645M
- Online Computer Library Center (OCLC) ID: 34708904
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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12Methodology for sensitivity analysis, approximate analysis, and design optimization in CFD for multidisciplinary applications
By Arthur C. Taylor
“Methodology for sensitivity analysis, approximate analysis, and design optimization in CFD for multidisciplinary applications” Metadata:
- Title: ➤ Methodology for sensitivity analysis, approximate analysis, and design optimization in CFD for multidisciplinary applications
- Author: Arthur C. Taylor
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Old Dominion University Research Foundation - Dept. of Mechanical Engineering, College of Engineering & Technology, Old Dominion University
- Publish Date: 1992 - 1993 - 1994 - 1996
- Publish Location: ➤ Norfolk, Va - Springfield, Va - [Washington, DC - [Springfield, Va - [Washington, D.C
“Methodology for sensitivity analysis, approximate analysis, and design optimization in CFD for multidisciplinary applications” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Airfoils - Algorithms - Architecture (Computers) - Computational fluid dynamics - Design analysis - Iterative solution - Linear equations - Matrices (Mathematics) - Memory (Computers) - Navier-Stokes equation - Optimization - Sensitivity - Software tools - Supersonic flow - Turbulent flows - Viscous flow
Edition Identifiers:
- The Open Library ID: OL15359487M - OL17030214M - OL15402708M - OL15498963M
- Online Computer Library Center (OCLC) ID: 32752276
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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13Two-dimensional high-lift aerodynamic optimization using neural networks
By Roxana M. Greenman
“Two-dimensional high-lift aerodynamic optimization using neural networks” Metadata:
- Title: ➤ Two-dimensional high-lift aerodynamic optimization using neural networks
- Author: Roxana M. Greenman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ Springfield, Va - Moffett Field, Calif
“Two-dimensional high-lift aerodynamic optimization using neural networks” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Computers - Navier-Stokes equation - Lift - Neural nets - Airfoils - Aerodynamic configurations - Angle of attack - Incompressible flow
Edition Identifiers:
- The Open Library ID: OL17129961M - OL17580142M - OL18132744M - OL15542052M
- Online Computer Library Center (OCLC) ID: 41151565
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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14On central-difference and upwind schemes
By R. Charles Swanson
“On central-difference and upwind schemes” Metadata:
- Title: ➤ On central-difference and upwind schemes
- Author: R. Charles Swanson
- Language: English
- Number of Pages: Median: 40
- Publisher: ➤ For sale by the National Technical Information Service - Institute for Computer Applications in Science and Engineering - National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering
- Publish Date: 1990
- Publish Location: Hampton, Va - [Springfield, Va
“On central-difference and upwind schemes” Subjects and Themes:
- Subjects: ➤ Airfoils - Central differencing - Dissipation - Mathematical models - TVD schemes - Upwind schemes
Edition Identifiers:
- The Open Library ID: OL18240517M - OL16129006M - OL17628297M - OL21333229M
- Online Computer Library Center (OCLC) ID: 61695882
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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15A 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
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16Two-dimensional aerodynamic characteristics of the OLS/TAAT airfoil
By Michael E. Watts
“Two-dimensional aerodynamic characteristics of the OLS/TAAT airfoil” Metadata:
- Title: ➤ Two-dimensional aerodynamic characteristics of the OLS/TAAT airfoil
- Author: Michael E. Watts
- Language: English
- Number of Pages: Median: 88
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Division - Ames Research Center
- Publish Date: 1988 - 1989
- Publish Location: ➤ [Washington, DC] - Moffett Field, Va
“Two-dimensional aerodynamic characteristics of the OLS/TAAT airfoil” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL18031874M - OL15285021M - OL20898425M - OL17098621M
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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17A transonic-small-disturbance wing design methodology
By Pamela S. Phillips
“A transonic-small-disturbance wing design methodology” Metadata:
- Title: ➤ A transonic-small-disturbance wing design methodology
- Author: Pamela S. Phillips
- Language: English
- Number of Pages: Median: 28
- Publisher: ➤ Langley Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Division - For sale by the National Technical Information Service]
- Publish Date: 1988
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, DC]
“A transonic-small-disturbance wing design methodology” Subjects and Themes:
- Subjects: Wings - Airplanes - Transonic flow - Airfoils
Edition Identifiers:
- The Open Library ID: OL18028135M - OL14662165M - OL15273068M - OL19253410M
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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18Evaluation of constant-Weber-number scaling for icing tests
By David N. Anderson
“Evaluation of constant-Weber-number scaling for icing tests” Metadata:
- Title: ➤ Evaluation of constant-Weber-number scaling for icing tests
- Author: David N. Anderson
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Evaluation of constant-Weber-number scaling for icing tests” Subjects and Themes:
- Subjects: Ice formation - Airfoils - Ice
Edition Identifiers:
- The Open Library ID: OL17117421M - OL15423306M - OL17106518M - OL18086933M
- Online Computer Library Center (OCLC) ID: 35224562
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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19Low-speed wind-tunnel results for symmetrical NASA LS(1)-0013 airfoil
By James C. Ferris
“Low-speed wind-tunnel results for symmetrical NASA LS(1)-0013 airfoil” Metadata:
- Title: ➤ Low-speed wind-tunnel results for symmetrical NASA LS(1)-0013 airfoil
- Author: James C. Ferris
- Language: English
- Number of Pages: Median: 35
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Office - Langley Research Center - For sale by the National Technical Information Service]
- Publish Date: 1987
- Publish Location: ➤ [Washington, DC] - Hampton, Va - [Springfield, Va
“Low-speed wind-tunnel results for symmetrical NASA LS(1)-0013 airfoil” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL18032411M - OL15287462M - OL19246800M - OL17099218M
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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20Distributed-roughness effects on stability and transition in swept-wing boundary layers
By Ruben B. Carrillo
“Distributed-roughness effects on stability and transition in swept-wing boundary layers” Metadata:
- Title: ➤ Distributed-roughness effects on stability and transition in swept-wing boundary layers
- Author: Ruben B. Carrillo
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Distributed-roughness effects on stability and transition in swept-wing boundary layers” Subjects and Themes:
- Subjects: ➤ Airfoils - Boundary layer stability - Boundary layer transition - Cross flow - Flow visualization - Surface roughness - Swept wings - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17128387M - OL17597200M - OL18132177M - OL15540242M
- Online Computer Library Center (OCLC) ID: 40717111
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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21Key topics for high-lift research
By David Fisher
“Key topics for high-lift research” Metadata:
- Title: ➤ Key topics for high-lift research
- Author: David Fisher
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Key topics for high-lift research” Subjects and Themes:
- Subjects: ➤ F-15 aircraft - Aerodynamics - Fins - Flow distribution - Lift - Airfoils - Wind tunnel tests - Flight tests
Edition Identifiers:
- The Open Library ID: OL17565560M - OL15492341M - OL17124491M - OL18116300M
- Online Computer Library Center (OCLC) ID: 39517789
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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22Two-dimensional aerodynamic characteristics of the NACA 0012 airfoil in the Langley 8-foot transonic pressure tunnel
By Charles D. Harris
“Two-dimensional aerodynamic characteristics of the NACA 0012 airfoil in the Langley 8-foot transonic pressure tunnel” Metadata:
- Title: ➤ Two-dimensional aerodynamic characteristics of the NACA 0012 airfoil in the Langley 8-foot transonic pressure tunnel
- Author: Charles D. Harris
- Number of Pages: Median: 137
- Publisher: Langley Research Center
- Publish Date: 1981
- Publish Location: Hampton, Va
“Two-dimensional aerodynamic characteristics of the NACA 0012 airfoil in the Langley 8-foot transonic pressure tunnel” Subjects and Themes:
- Subjects: Aerodynamic characteristics - Airfoils - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL19750282M - OL21333674M
Access and General Info:
- First Year Published: 1981
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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23Control 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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24Higher-order approximations in interactive airfoil calculations
By D. W. Zingg
“Higher-order approximations in interactive airfoil calculations” Metadata:
- Title: ➤ Higher-order approximations in interactive airfoil calculations
- Author: D. W. Zingg
- Language: English
- Number of Pages: Median: 102
- Publisher: ➤ University of Toronto - Institute for Aerospace Studies
- Publish Date: 1987 - 1988
- Publish Location: [Downsview, Ont.]
“Higher-order approximations in interactive airfoil calculations” Subjects and Themes:
- Subjects: ➤ Airfoils - Boundary layers - Computational fluid dynamics - Incompressible flow - Interactive methods - Pressure gradients - Subsonic flow
Edition Identifiers:
- The Open Library ID: OL20898250M - OL19987220M - OL20697434M
Author's Alternative Names:
"David W. Zingg"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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25TADS, a CFD-based turbomachinery and analysis design system with GUI
By D. A. Topp
“TADS, a CFD-based turbomachinery and analysis design system with GUI” Metadata:
- Title: ➤ TADS, a CFD-based turbomachinery and analysis design system with GUI
- Author: D. A. Topp
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“TADS, a CFD-based turbomachinery and analysis design system with GUI” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - User manuals (Computer programs) - Three dimensional flow - Computer systems programs - Turbomachinery - Turbomachine blades - Systems analysis - Grid generation (Mathematics) - Computer systems design - Computer aided design - Graphical user interface - Cascade flow - Design analysis - Applications programs (Computers) - Airfoils
Edition Identifiers:
- The Open Library ID: OL15423412M - OL18086968M - OL17107731M
- Online Computer Library Center (OCLC) ID: 35241867
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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26Wing-section optimization for supersonic viscous flow
By Cem C. Item
“Wing-section optimization for supersonic viscous flow” Metadata:
- Title: ➤ Wing-section optimization for supersonic viscous flow
- Author: Cem C. Item
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Wing-section optimization for supersonic viscous flow” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Viscous flow - Mathematical models - Supersonic flow - Aicraft design - Navier-Stokes equation - Airfoils - Aerodynamic configurations - Two dimensional models - Computer aided design
Edition Identifiers:
- The Open Library ID: OL17078554M - OL18084623M - OL15419484M
- Online Computer Library Center (OCLC) ID: 34608891
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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27SiC/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
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28A computionally efficient modelling of laminar separation bubbles
By Paolo Dini
“A computionally efficient modelling of laminar separation bubbles” Metadata:
- Title: ➤ A computionally efficient modelling of laminar separation bubbles
- Author: Paolo Dini
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Dept. of Aerospace Engineering, Pennsylvania State University
- Publish Date: 1989 - 1990
- Publish Location: ➤ University Park, PA - [Springfield, Va - [Washington, DC
“A computionally efficient modelling of laminar separation bubbles” Subjects and Themes:
- Subjects: ➤ Laminar flow - Computer simulation - Aerofoils - Separated flow - Aerodynamics - Flow characteristics - Prediction analysis techniques - Mathematical models - Bubbles - Airfoils
Edition Identifiers:
- The Open Library ID: OL15396669M - OL15277898M - OL15407502M
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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29The semi-discrete Galerkin finite element modelling of compressible viscous flow past an airfoil
By Andrew J. Meade
“The semi-discrete Galerkin finite element modelling of compressible viscous flow past an airfoil” Metadata:
- Title: ➤ The semi-discrete Galerkin finite element modelling of compressible viscous flow past an airfoil
- Author: Andrew J. Meade
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1992
- Publish Location: ➤ Springfield, Va - [Washington, DC
“The semi-discrete Galerkin finite element modelling of compressible viscous flow past an airfoil” Subjects and Themes:
- Subjects: ➤ Boundary layer equations - Viscous flow - Galerkin method - Compressible flow - Airfoils - Mathematical models - Finite element method
Edition Identifiers:
- The Open Library ID: OL15404705M - OL17030205M - OL18076706M
- Online Computer Library Center (OCLC) ID: 32339159
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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30The 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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31Domain decomposition for aerodynamic and aeroacoustic analyses, and optimization
By Oktay Baysal
“Domain decomposition for aerodynamic and aeroacoustic analyses, and optimization” Metadata:
- Title: ➤ Domain decomposition for aerodynamic and aeroacoustic analyses, and optimization
- Author: Oktay Baysal
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Dept. of Aerospace Engineering, College of Engineering & Technology, Old Dominion University - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, D.C - Norfolk, Va
“Domain decomposition for aerodynamic and aeroacoustic analyses, and optimization” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Aerodynamic characteristics - Airfoils - Cavity flow - Computational fluid dynamics - Partial Differential equations - Unstructured grids (Mathematics)
Edition Identifiers:
- The Open Library ID: OL17796518M - OL15423196M
- Online Computer Library Center (OCLC) ID: 35268604
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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32ICEG2D (v2.0)
By David Thompson
“ICEG2D (v2.0)” Metadata:
- Title: ICEG2D (v2.0)
- Author: David Thompson
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - NASA Center for Aerospace Information
- Publish Date: 2001
- Publish Location: ➤ Hanover, MD - [Cleveland, Ohio]
“ICEG2D (v2.0)” Subjects and Themes:
- Subjects: ➤ Computerized simulation - Aircraft icing - Ice formation - Software development tools - Applications programs (Computers) - Flow distribution - Computational fluid dymanics - Algorithms - Airfoils - Prediction analysis techniques - Computer programs
Edition Identifiers:
- The Open Library ID: OL17612548M - OL21310195M
- Online Computer Library Center (OCLC) ID: 52061314
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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33EUROPT-a European initiative on optimum design methods in dynamics
By Brite/Euram Project Workshop "Optimum Design in Aerodynamics" (1992 Barcelona, Spain)
“EUROPT-a European initiative on optimum design methods in dynamics” Metadata:
- Title: ➤ EUROPT-a European initiative on optimum design methods in dynamics
- Author: ➤ Brite/Euram Project Workshop "Optimum Design in Aerodynamics" (1992 Barcelona, Spain)
- Language: English
- Number of Pages: Median: 196
- Publisher: ➤ Friedrich Vieweg & Sohn Verlag - Vieweg
- Publish Date: 1997
- Publish Location: Braunschweig
“EUROPT-a European initiative on optimum design methods in dynamics” Subjects and Themes:
- Subjects: ➤ Congresses - Mathematics - Aerodynamics - Airfoils - Mathematical models - Aerofoils
Edition Identifiers:
- The Open Library ID: OL9053135M - OL282870M
- Library of Congress Control Number (LCCN): 97185296
- All ISBNs: 3528076550 - 9783528076559
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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34Potential flow around two-dimensional airfoils using a singular integral method
By Yves Nguyen
“Potential flow around two-dimensional airfoils using a singular integral method” Metadata:
- Title: ➤ Potential flow around two-dimensional airfoils using a singular integral method
- Author: Yves Nguyen
- Language: English
- Number of Pages: Median: 99
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - Fluid Dynamics Group, Bureau of Engineering Research, University of Texas at Austin
- Publish Date: 1987
- Publish Location: ➤ [Washington, D.C - Springfield, Va - Austin, TX
“Potential flow around two-dimensional airfoils using a singular integral method” Subjects and Themes:
- Subjects: ➤ Aerofoils - Singular integrals - Fluid mechanics - Two dimensional bodies - Airfoils - Potential flow - Singular integral equations
Edition Identifiers:
- The Open Library ID: OL14980155M - OL17683676M
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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35Control of flow separation and mixing by aerodynamic excitation
By Edward J. Rice
“Control of flow separation and mixing by aerodynamic excitation” Metadata:
- Title: ➤ Control of flow separation and mixing by aerodynamic excitation
- Author: Edward J. Rice
- Language: English
- Number of Pages: Median: 11
- Publisher: ➤ NASA - For sale by the National Technical Information Service
- Publish Date: 1990
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Control of flow separation and mixing by aerodynamic excitation” Subjects and Themes:
- Subjects: ➤ Shear flow - Inlet flow - Shear layers - Separated flow - Boundary layer separation - Coanda effect - Engine inlets - Aircraft engines - Airfoils - Mixing - Turbulence effects - Unsteady aerodynamics
Edition Identifiers:
- The Open Library ID: OL16135113M - OL17634399M
- Online Computer Library Center (OCLC) ID: 24985892
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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36An approach to the design of airfoils with high lift to drag ratios
By D. W. Zingg
“An approach to the design of airfoils with high lift to drag ratios” Metadata:
- Title: ➤ An approach to the design of airfoils with high lift to drag ratios
- Author: D. W. Zingg
- Number of Pages: Median: 59
- Publisher: ➤ Institute for Aerospace Studies - Dept. of Aerospace Science and Engineering
- Publish Date: 1981 - 1983
- Publish Location: [Downsview, Ont.]
“An approach to the design of airfoils with high lift to drag ratios” Subjects and Themes:
- Subjects: Lift drag ratio - Airfoils - Panel method
Edition Identifiers:
- The Open Library ID: OL20968289M - OL19988674M
Author's Alternative Names:
"David W. Zingg"Access and General Info:
- First Year Published: 1981
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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37Grid studies for thin-layer Navier-Stokes computations of airfoil flowfields
By D. W. Zingg
“Grid studies for thin-layer Navier-Stokes computations of airfoil flowfields” Metadata:
- Title: ➤ Grid studies for thin-layer Navier-Stokes computations of airfoil flowfields
- Author: D. W. Zingg
- Number of Pages: Median: 1288
- Publisher: ➤ Sine nomine - American Institute of Aeronautics and Astronautics
- Publish Date: 1992
- Publish Location: [S.l.] - Washington, D. C
“Grid studies for thin-layer Navier-Stokes computations of airfoil flowfields” Subjects and Themes:
- Subjects: Computational grids - Navier-Stokes equation - Transonic flow - Flow distribution - Airfoils
Edition Identifiers:
- The Open Library ID: OL19246870M - OL19047112M
Author's Alternative Names:
"David W. Zingg"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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38Interactive airfoil calculations with higher-order viscous flow equations
By D. W. Zingg
“Interactive airfoil calculations with higher-order viscous flow equations” Metadata:
- Title: ➤ Interactive airfoil calculations with higher-order viscous flow equations
- Author: D. W. Zingg
- Number of Pages: Median: 526
- Publisher: ➤ American Institute of Aeronautics and Astronautics - American Institute of Aeronautics & Astronautics
- Publish Date: 1990 - 1991
- Publish Location: Washington, D. C
“Interactive airfoil calculations with higher-order viscous flow equations” Subjects and Themes:
- Subjects: Viscous flow - Airfoils
Edition Identifiers:
- The Open Library ID: OL21499746M - OL19046258M
Author's Alternative Names:
"David W. Zingg"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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39Active control of flow separation over an airfoil
By S. S. Ravindran
“Active control of flow separation over an airfoil” Metadata:
- Title: ➤ Active control of flow separation over an airfoil
- Author: S. S. Ravindran
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: Springfield, VA - Hampton, Va
“Active control of flow separation over an airfoil” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Separated flow - Mathematical models - Navier-Stokes equation - Algorithms - Airfoils - Active control - Unsteady aerodynamics
Edition Identifiers:
- The Open Library ID: OL17602493M - OL17703416M
- Online Computer Library Center (OCLC) ID: 44140453
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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40Experimental study of complex vortex interactions in the wake of high aspect ratio wings
By Ömer Savas
“Experimental study of complex vortex interactions in the wake of high aspect ratio wings” Metadata:
- Title: ➤ Experimental study of complex vortex interactions in the wake of high aspect ratio wings
- Author: Ömer Savas
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Experimental study of complex vortex interactions in the wake of high aspect ratio wings” Subjects and Themes:
- Subjects: ➤ Particle image velocimetry - Time measurement - Airfoils - Wakes - Vortices - Wind tunnels - Wings
Edition Identifiers:
- The Open Library ID: OL17132865M - OL17583308M
- Online Computer Library Center (OCLC) ID: 41969386
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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41Study of large-scale mixing in developing wakes behind streamlined bodies
By B. R. Ramaprian
“Study of large-scale mixing in developing wakes behind streamlined bodies” Metadata:
- Title: ➤ Study of large-scale mixing in developing wakes behind streamlined bodies
- Author: B. R. Ramaprian
- Language: English
- Publisher: ➤ Iowa Institute of Hydraulic Research, the University of Iowa - NASA Ames Research Center
- Publish Date: 1984
- Publish Location: ➤ [Moffett Field, Calif - Iowa City, Iowa
“Study of large-scale mixing in developing wakes behind streamlined bodies” Subjects and Themes:
- Subjects: ➤ Wakes (Fluid dynamics) - Boundary layers - Streamlined bodies - Two dimensional flow - Near wakes - Airfoils - Mixing - Wakes (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL16154757M - OL18293349M
Access and General Info:
- First Year Published: 1984
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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42Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program
By Bruce Charles
“Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program” Metadata:
- Title: ➤ Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program
- Author: Bruce Charles
- 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
“Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program” Subjects and Themes:
- Subjects: ➤ Trailing edge flaps - Airfoils - Noise pollution - Aerodynamic loads - Dynamic characteristics - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL17591432M - OL15552422M
- Online Computer Library Center (OCLC) ID: 42623818
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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43Multi-element airfoil optimization for maximum lift at high Reynolds numbers
By Walter O. Valarezo
“Multi-element airfoil optimization for maximum lift at high Reynolds numbers” Metadata:
- Title: ➤ Multi-element airfoil optimization for maximum lift at high Reynolds numbers
- Author: Walter O. Valarezo
- Language: English
- Number of Pages: Median: 976
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1991
- Publish Location: New York
“Multi-element airfoil optimization for maximum lift at high Reynolds numbers” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL19243245M - OL20379435M
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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44Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil
By Dale Ashby
“Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil” Metadata:
- Title: ➤ Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil
- Author: Dale Ashby
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - Joint Institute for Aeronautics and Acoustics, Stanford University - National Technical Information Service, distributor - Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1996
- Publish Location: ➤ [Stanford, Calif.] - [Washington, DC - Springfield, Va
“Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Airfoils - Boundary layer separation - Flaps (Control surfaces) - Incompressible flow - Lift augmentation - Potential flow - Pressure distribution - Separated flow - Tabs (Control surfaces)
Edition Identifiers:
- The Open Library ID: OL15505042M - OL17838000M
- Online Computer Library Center (OCLC) ID: 40101894
Access and General Info:
- First Year Published: 1996
- 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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45Wing-section optimization for supersonic viscous flows
By Cem C. Item
“Wing-section optimization for supersonic viscous flows” Metadata:
- Title: ➤ Wing-section optimization for supersonic viscous flows
- Author: Cem C. Item
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Wing-section optimization for supersonic viscous flows” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Aerodynamic configurations - Aicraft design - Airfoils - Applications programs (Computers) - Computational fluid dynamics - Inviscid flow - Navier-Stokes equation - Optimization - Supersonic flow - Viscous flow
Edition Identifiers:
- The Open Library ID: OL18084626M - OL17078549M
- Online Computer Library Center (OCLC) ID: 34609263
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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46ICEG2D (v2.0)
By David S. Thompson
“ICEG2D (v2.0)” Metadata:
- Title: ICEG2D (v2.0)
- Author: David S. Thompson
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - NASA Center for Aerospace Information
- Publish Date: 2001
- Publish Location: ➤ [Cleveland, Ohio] - Hanover, MD
“ICEG2D (v2.0)” Subjects and Themes:
- Subjects: ➤ Computerized simulation - Aircraft icing - Ice formation - Software development tools - Applications programs (Computers) - Flow distribution - Computational fluid dymanics - Algorithms - Airfoils - Prediction analysis techniques - Computer programs
Edition Identifiers:
- The Open Library ID: OL16025835M - OL18167712M
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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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47SmaggIce user guide
By Marivell Baez
“SmaggIce user guide” Metadata:
- Title: SmaggIce user guide
- Author: Marivell Baez
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - National Technical Information Service [distributor - Available from NASA Center for Aerospace Information
- Publish Date: 2000
- Publish Location: ➤ Springfield, VA - Hanover, MD - Cleveland, Ohio
“SmaggIce user guide” Subjects and Themes:
- Subjects: ➤ Aircraft icing - Airfoils - Computational fluid dynamics - Grid generation (Mathematics) - Software development tools - User manuals (Computer programs)
Edition Identifiers:
- The Open Library ID: OL17595004M - OL15568039M
- Online Computer Library Center (OCLC) ID: 44122585
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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48Three-dimensional aerodynamic shape optimization using discrete sensitivity analysis
By Gregory Wayne Burgreen
“Three-dimensional aerodynamic shape optimization using discrete sensitivity analysis” Metadata:
- Title: ➤ Three-dimensional aerodynamic shape optimization using discrete sensitivity analysis
- Author: Gregory Wayne Burgreen
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“Three-dimensional aerodynamic shape optimization using discrete sensitivity analysis” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Supersonic nozzles - Sensitivity - Delta wings - Discrete functions - Airfoils - Aerodynamic configurations - Aircraft design - Supercritical wings - Computer aided design
Edition Identifiers:
- The Open Library ID: OL15419545M - OL18084662M
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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49Wall interference tests of a CAST 10-2/DOA 2 airfoil in an adaptive-wall test section
By Raymond E. Mineck
“Wall interference tests of a CAST 10-2/DOA 2 airfoil in an adaptive-wall test section” Metadata:
- Title: ➤ Wall interference tests of a CAST 10-2/DOA 2 airfoil in an adaptive-wall test section
- Author: Raymond E. Mineck
- Language: English
- Number of Pages: Median: 96
- Publisher: ➤ Langley Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Division
- Publish Date: 1987 - 1988
- Publish Location: Hampton, Va - [Washington, DC]
“Wall interference tests of a CAST 10-2/DOA 2 airfoil in an adaptive-wall test section” Subjects and Themes:
- Subjects: ➤ Airfoils - Aerodynamics - Correction - Interference - Wind tunnel walls - Aerofoils
Edition Identifiers:
- The Open Library ID: OL19250365M - OL15278226M
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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50The status of two-dimensional testing at high transonic speeds in the University of Southampton transonic self-streamlining wind tunnel
By M. C. Lewis
“The status of two-dimensional testing at high transonic speeds in the University of Southampton transonic self-streamlining wind tunnel” Metadata:
- Title: ➤ The status of two-dimensional testing at high transonic speeds in the University of Southampton transonic self-streamlining wind tunnel
- Author: M. C. Lewis
- 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, DC] - [Springfield, Va
“The status of two-dimensional testing at high transonic speeds in the University of Southampton transonic self-streamlining wind tunnel” Subjects and Themes:
- Subjects: ➤ Universities - Transonic wind tunnels - Streamlining - Airfoils - Wind tunnel tests - Wind tunnel walls
Edition Identifiers:
- The Open Library ID: OL15416389M - OL18082743M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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