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Source: The Open Library
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1Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code
By Wendy B. Lessard
“Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code” Metadata:
- Title: ➤ Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code
- Author: Wendy B. Lessard
- Language: English
- Number of Pages: Median: 77
- Publisher: ➤ Available from the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ Hampton, Va - Springfield, VA - [Springfield, Va
“Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Aircraft models - Pressure distribution - Subsonic flow - Unstructured grids (Mathematics) - Angle of attack - Grid generation (Mathematics) - Flow distribution - Aerodynamics - F-16 (Jet fighter plane) - Wind tunnel models - Mathematics - Numerical grid generation (Numerical analysis)
Edition Identifiers:
- The Open Library ID: OL18121254M - OL17581026M - OL19045641M - OL15504440M - OL17126971M
- Online Computer Library Center (OCLC) ID: 40389824
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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22-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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3High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation
By Robert S. Jankovsky
“High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation” Metadata:
- Title: ➤ High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation
- Author: Robert S. Jankovsky
- Language: English
- Number of Pages: Median: 51
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 1999
- Publish Location: ➤ [Springfield, Va - [Cleveland, Ohio]
“High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation” Subjects and Themes:
- Subjects: ➤ Combustion chambers - Turbulence - Heat transfer - Boundary layer thickness - Heat flux - Rocket nozzles - Flux (Rate) - Pressure distribution - Pressure measurement - Measurement - Transmission - Boundary layer - Rocket engines - Nozzles - Pressure - Heat - Aerodynamic load
Edition Identifiers:
- The Open Library ID: OL17591578M - OL15556459M - OL18137669M - OL20703973M - OL17136005M
- Online Computer Library Center (OCLC) ID: 42885454
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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4F-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
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5Laser scanning system for pressure and temperature paints
By John Sullivan
“Laser scanning system for pressure and temperature paints” Metadata:
- Title: ➤ Laser scanning system for pressure and temperature paints
- Author: John Sullivan
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Laser scanning system for pressure and temperature paints” Subjects and Themes:
- Subjects: ➤ Pressure distribution - Paints - Aerospace vehicles - Spatial resolution - High resolution - Pressure measurement - Control surfaces - Aerodynamics
Edition Identifiers:
- The Open Library ID: OL17837386M - OL17697854M - OL17126090M
- Online Computer Library Center (OCLC) ID: 40109522
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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6Rocket-based combined cycle engine technology development
By J. R. DeBonis
“Rocket-based combined cycle engine technology development” Metadata:
- Title: ➤ Rocket-based combined cycle engine technology development
- Author: J. R. DeBonis
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center, Ohio Aerospace Institute, Institute for Computational Mechanics in Propulsion - National Aeronautics and Space Administration, distributor]
- Publish Date: 1996
- Publish Location: ➤ [Cleveland, Ohio] - [Springfield, Va
“Rocket-based combined cycle engine technology development” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Computational grids - Engine inlets - Flow distribution - Hypersonic flow - Navier-Stokes equation - Pressure distribution - Rocket engine design - Rocket engines - Static pressure
Edition Identifiers:
- The Open Library ID: OL17593984M - OL18121288M - OL15504564M
- Online Computer Library Center (OCLC) ID: 41375980
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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7Simulation of real-gas effects on pressure distributions for aeroassist flight experiment vehicle and comparison with prediction
By John R. Micol
“Simulation of real-gas effects on pressure distributions for aeroassist flight experiment vehicle and comparison with prediction” Metadata:
- Title: ➤ Simulation of real-gas effects on pressure distributions for aeroassist flight experiment vehicle and comparison with prediction
- Author: John R. Micol
- Language: English
- Number of Pages: Median: 67
- Publisher: ➤ Langley Research Center - For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1992
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, DC]
“Simulation of real-gas effects on pressure distributions for aeroassist flight experiment vehicle and comparison with prediction” Subjects and Themes:
- Subjects: ➤ Aeroassist Flight Experiment - Aerodynamics, Hypersonic - Gases, Real - Hypersonic Aerodynamics - Pressure distribution - Real Gases
Edition Identifiers:
- The Open Library ID: OL15357049M - OL19243164M - OL18052286M
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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8Measurements of unsteady pressure and structural response for an elastic supercritical wing
By Clinton V. Eckstrom
“Measurements of unsteady pressure and structural response for an elastic supercritical wing” Metadata:
- Title: ➤ Measurements of unsteady pressure and structural response for an elastic supercritical wing
- Author: Clinton V. Eckstrom
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - For sale by the National Technical Information Service
- Publish Date: 1994
- Publish Location: ➤ Hampton - Hampton, Va - [Springfield, Va
“Measurements of unsteady pressure and structural response for an elastic supercritical wing” Subjects and Themes:
- Subjects: ➤ Aeroelasticity - Dynamic response - Pressure distribution - Supercritical wings - Transonic speed - Unsteady flow - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15410960M - OL17790670M - OL22824033M
- Online Computer Library Center (OCLC) ID: 32863973
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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9Analysis of two-phase flow in damper seals for cryogenic turbomachinery
By Grigory L. Arauz
“Analysis of two-phase flow in damper seals for cryogenic turbomachinery” Metadata:
- Title: ➤ Analysis of two-phase flow in damper seals for cryogenic turbomachinery
- Author: Grigory L. Arauz
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - Texas A&M University, Mechanical Engineering Dept. - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC - [College Station, Tex.] - Springfield, Va
“Analysis of two-phase flow in damper seals for cryogenic turbomachinery” Subjects and Themes:
- Subjects: ➤ Two phase flow - Pressure distribution - Liquid-vapor interfaces - Turbomachinery - Seals (Stoppers) - Rotor dynamics - Leakage - Fluid pressure
Edition Identifiers:
- The Open Library ID: OL18122158M - OL17132882M - OL15507984M
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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10Enhanced design of turbo-jet LPT by separation control using phased plasma actuators
By Thomas C. Corke
“Enhanced design of turbo-jet LPT by separation control using phased plasma actuators” Metadata:
- Title: ➤ Enhanced design of turbo-jet LPT by separation control using phased plasma actuators
- Author: Thomas C. Corke
- Language: English
- Publisher: ➤ National Technical Information Service [distributor - Available from NASA Center for Aerospace Administration - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2003
- Publish Location: ➤ Springfield, VA - Hanover, MD - [Cleveland, Ohio]
“Enhanced design of turbo-jet LPT by separation control using phased plasma actuators” Subjects and Themes:
- Subjects: ➤ Actuators - Boundary layer separation - Computational fluid dynamics - Flow distribution - Pressure distribution - Reattached flow - Separated flow - Turbine blades
Edition Identifiers:
- The Open Library ID: OL17633155M - OL18205099M - OL16094177M
- Online Computer Library Center (OCLC) ID: 56823171
Access and General Info:
- First Year Published: 2003
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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11An edge-based solution-adaptive method applied to the AIRPLANE code
By Rupak Biswas
“An edge-based solution-adaptive method applied to the AIRPLANE code” Metadata:
- Title: ➤ An edge-based solution-adaptive method applied to the AIRPLANE code
- Author: Rupak Biswas
- Language: English
- Publisher: ➤ Research Institute for Advanced Computer Science, NASA Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Moffett Field, CA]
“An edge-based solution-adaptive method applied to the AIRPLANE code” Subjects and Themes:
- Subjects: ➤ Pressure distribution - Transonic flow - Near fields - Unstructured grids (Mathematics) - Flow distribution - Aircraft configurations - Sonic booms - Grid generation (Mathematics) - Supersonic flow - Shock waves
Edition Identifiers:
- The Open Library ID: OL15419501M - OL18084638M
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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12Solar rocket plume/mirror interactions
By Sheng-Tao Yu
“Solar rocket plume/mirror interactions” Metadata:
- Title: ➤ Solar rocket plume/mirror interactions
- Author: Sheng-Tao Yu
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration
- Publish Date: 1991
- Publish Location: [Washington, D.C.]
“Solar rocket plume/mirror interactions” Subjects and Themes:
- Subjects: ➤ Boundary layer transition - Continuums - Fouling - Hydrogen fuels - Navier-Stokes equation - Pressure distribution - Pressure effects - Solar thermal propulsion - Viscous flow
Edition Identifiers:
- The Open Library ID: OL17632392M - OL16133038M
- Online Computer Library Center (OCLC) ID: 63906446
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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13Experimental 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
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14Evaluation of 3D inverse code using rotor 67 as test case
By T. Dang
“Evaluation of 3D inverse code using rotor 67 as test case” Metadata:
- Title: ➤ Evaluation of 3D inverse code using rotor 67 as test case
- Author: T. Dang
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1998
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Evaluation of 3D inverse code using rotor 67 as test case” Subjects and Themes:
- Subjects: Inviscid flow - Rotors - Computer programs - Pressure distribution - Pressure
Edition Identifiers:
- The Open Library ID: OL15543277M - OL17597306M
- Online Computer Library Center (OCLC) ID: 41363696
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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15Experimental aerothermodynamic research of hypersonic aircraft
By Joseph W. Cleary
“Experimental aerothermodynamic research of hypersonic aircraft” Metadata:
- Title: ➤ Experimental aerothermodynamic research of hypersonic aircraft
- Author: Joseph W. Cleary
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1987 - 1989
- Publish Location: ➤ Springfield, Va.? - [Washington, DC
“Experimental aerothermodynamic research of hypersonic aircraft” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Pressure distribution - Afterbodies - Forebodies - Flow distribution - Aerothermodynamics - Hypersonic aircraft - Wind tunnel models - Aerodynamic configurations
Edition Identifiers:
- The Open Library ID: OL15398951M - OL15408376M
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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16Effects of winglets on a first-generation jet transport wing
By Robert R. Meyer
“Effects of winglets on a first-generation jet transport wing” Metadata:
- Title: ➤ Effects of winglets on a first-generation jet transport wing
- Author: Robert R. Meyer
- Language: English
- Number of Pages: Median: 56
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service] - Dryden Flight Research Facility
- Publish Date: 1986
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va - Edwards, Calif
“Effects of winglets on a first-generation jet transport wing” Subjects and Themes:
- Subjects: ➤ Sideslip - Pressure distribution - Winglets - Airplanes - Wing loading - Wings
Edition Identifiers:
- The Open Library ID: OL20984694M - OL14662608M
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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17Pressure distributions from subsonic tests of a NACA 0012 semispan wing model
By Zachary T. Applin
“Pressure distributions from subsonic tests of a NACA 0012 semispan wing model” Metadata:
- Title: ➤ Pressure distributions from subsonic tests of a NACA 0012 semispan wing model
- Author: Zachary T. Applin
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: Hampton, Va - [Springfield, Va
“Pressure distributions from subsonic tests of a NACA 0012 semispan wing model” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Airfoil profiles - Dynamic pressure - Free flow - Pressure distribution - Semispan models - Subsonic speed - Unswept wings - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15421506M - OL17794166M
- Online Computer Library Center (OCLC) ID: 35231688
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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18Wing pressure distributions from subsonic tests of a high-wing transport model
By Zachary T. Applin
“Wing pressure distributions from subsonic tests of a high-wing transport model” Metadata:
- Title: ➤ Wing pressure distributions from subsonic tests of a high-wing transport model
- Author: Zachary T. Applin
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: Hampton, Va - [Springfield, Va
“Wing pressure distributions from subsonic tests of a high-wing transport model” Subjects and Themes:
- Subjects: ➤ Angle of attack - Leading edge flaps - Mach number - Pressure distribution - Reynolds number - Sideslip - Subsonic flow - Trailing edge flaps - Transport aircraft - Wind tunnel tests - Wings
Edition Identifiers:
- The Open Library ID: OL17788775M - OL15411003M
- Online Computer Library Center (OCLC) ID: 32865600
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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19Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
By William G. Johnson
“Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel” Metadata:
- Title: ➤ Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
- Author: William G. Johnson
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1985
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel” Subjects and Themes:
- Subjects: ➤ Aerodynamics, Transonic - Aerofoils - Airfoil profiles - Boeing aircraft - Cryogenic wind tunnels - High Reynolds number - Pressure distribution - Reynolds number - Statistics - Supercritical airfoils - Testing - Transonic Aerodynamics - Two dimensional bodies - Wind tunnel models - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17727212M - OL17634944M
- Online Computer Library Center (OCLC) ID: 166902755
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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20Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing
By Sheryll Goecke Powers
“Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing” Metadata:
- Title: ➤ Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing
- Author: Sheryll Goecke Powers
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - National Technical Information Service, distributor]
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing” Subjects and Themes:
- Subjects: ➤ Boundary layers - Flight tests - Pressure distribution - Pressure measurement - Swept wings - Angle of attack - Reynolds number - Mach number - Supercritical wings
Edition Identifiers:
- The Open Library ID: OL17839404M - OL15548584M
- Online Computer Library Center (OCLC) ID: 41964681
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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21Computer code study of asteroid entry into Venusian atmosphere
By Robert M. Schmidt
“Computer code study of asteroid entry into Venusian atmosphere” Metadata:
- Title: ➤ Computer code study of asteroid entry into Venusian atmosphere
- Author: Robert M. Schmidt
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Computer code study of asteroid entry into Venusian atmosphere” Subjects and Themes:
- Subjects: ➤ Asteroids - Computer programs - Databases - Density (Mass/volume) - Pressure distribution - Venus atmosphere
Edition Identifiers:
- The Open Library ID: OL17597465M - OL15547927M
- Online Computer Library Center (OCLC) ID: 42334290
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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22Effect 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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23Calculation of multistage turbomachinery using steady characteristic boundary conditions
By Rodrick V. Chima
“Calculation of multistage turbomachinery using steady characteristic boundary conditions” Metadata:
- Title: ➤ Calculation of multistage turbomachinery using steady characteristic boundary conditions
- Author: Rodrick V. Chima
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration Langley Research Center - Available from National Technical Information Service
- Publish Date: 1998
- Publish Location: ➤ [Cleveland, Ohio] - Springfield, Va
“Calculation of multistage turbomachinery using steady characteristic boundary conditions” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Pressure distribution - Heat transfer coefficients - Turbulence models - Turbines - Finite difference theory - Navier-Stokes equation - Grid generation (Mathematics) - Multiblock grids
Edition Identifiers:
- The Open Library ID: OL17593118M - OL15543188M
- Online Computer Library Center (OCLC) ID: 41267349
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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24Atmospheric probe model
By Jerald M. Vogel
“Atmospheric probe model” Metadata:
- Title: Atmospheric probe model
- Author: Jerald M. Vogel
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1998
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Atmospheric probe model” Subjects and Themes:
- Subjects: ➤ Pressure distribution - Probes - Ring wings - Scale models - Velocity distribution - Wind tunnel models - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17595599M - OL15546934M
- Online Computer Library Center (OCLC) ID: 42695835
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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25Vibroacoustic response of pad structures to space shuttle launch acoustic loads
By R. N. Margasahayam
“Vibroacoustic response of pad structures to space shuttle launch acoustic loads” Metadata:
- Title: ➤ Vibroacoustic response of pad structures to space shuttle launch acoustic loads
- Author: R. N. Margasahayam
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Vibroacoustic response of pad structures to space shuttle launch acoustic loads” Subjects and Themes:
- Subjects: Pressure distribution - Random vibration - Vibrational stress - Acoustic fatigue - Launching pads
Edition Identifiers:
- The Open Library ID: OL17815468M - OL15484331M
- Online Computer Library Center (OCLC) ID: 38178091
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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26Coupling of low speed fan stator vane unsteady pressures to duct modes
By Daniel L. Sutliff
“Coupling of low speed fan stator vane unsteady pressures to duct modes” Metadata:
- Title: ➤ Coupling of low speed fan stator vane unsteady pressures to duct modes
- Author: Daniel L. Sutliff
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: ➤ Springfield, VA - [Cleveland, Ohio]
“Coupling of low speed fan stator vane unsteady pressures to duct modes” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Noise intensity - Pressure distribution - Predictions - Ducted fans - Aircraft noise - Rotor stator interactions - Engine noise - Green's functions
Edition Identifiers:
- The Open Library ID: OL15550581M - OL17584189M
- Online Computer Library Center (OCLC) ID: 42333114
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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27An analysis of the pressures, forces and moments induced by the ground vortex generated by a single impinging jet
By Richard E. Kuhn
“An analysis of the pressures, forces and moments induced by the ground vortex generated by a single impinging jet” Metadata:
- Title: ➤ An analysis of the pressures, forces and moments induced by the ground vortex generated by a single impinging jet
- Author: Richard E. Kuhn
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va
“An analysis of the pressures, forces and moments induced by the ground vortex generated by a single impinging jet” Subjects and Themes:
- Subjects: ➤ Ground effect (Aerodynamics) - Lift - Pitching moments - Pressure distribution - STOVL aircraft - Vortices - Wall jets
Edition Identifiers:
- The Open Library ID: OL15504968M
Author's Alternative Names:
"R. E. Kuhn"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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28Direct calculation of airfoils from pressure distribution
By Richard Eppler
“Direct calculation of airfoils from pressure distribution” Metadata:
- Title: ➤ Direct calculation of airfoils from pressure distribution
- Author: Richard Eppler
- Number of Pages: Median: 61
- Publisher: NASA
- Publish Date: 1974
- Publish Location: Washington, D. C
“Direct calculation of airfoils from pressure distribution” Subjects and Themes:
- Subjects: Airfoil profiles - Pressure distribution
Edition Identifiers:
- The Open Library ID: OL19916657M
Access and General Info:
- First Year Published: 1974
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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29Development of a variational SEASAT data analysis technique
By Yoshi K. Sasaki
“Development of a variational SEASAT data analysis technique” Metadata:
- Title: ➤ Development of a variational SEASAT data analysis technique
- Author: Yoshi K. Sasaki
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1986
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Development of a variational SEASAT data analysis technique” Subjects and Themes:
- Subjects: ➤ Radar measurement - Geostrophic wind - Satellite observation - Atmospheric boundary layer - Atmospheric pressure - Ocean surface - Pressure distribution - Algorithms - Calculus of variations - Wind velocity
Edition Identifiers:
- The Open Library ID: OL17684242M
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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30Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach
By W. P. Norby
“Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach” Metadata:
- Title: ➤ Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach
- Author: W. P. Norby
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Inlet flow - Computational grids - Pressure distribution - Turbulence models - Flow distortion - Flow distribution - Engine inlets - Aircraft engines - Angle of attack - Turbulence effects
Edition Identifiers:
- The Open Library ID: OL15490315M
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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31Airfoil 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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32Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf
By Milton Lamb
“Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf” Metadata:
- Title: ➤ Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf
- Author: Milton Lamb
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1996
- Publish Location: Hampton, Va - Springfield, VA
“Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf” Subjects and Themes:
- Subjects: ➤ Aircraft structures - Two dimensional flow - Pressure distribution - Afterburning - Static tests - Throats - Pressure ratio - Plumes - Nozzle design - Two dimensional models - Convergent-divergent nozzles
Edition Identifiers:
- The Open Library ID: OL15548582M
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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33Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the AEDC 16T propulsion wind tunnel
By Paul M. Siemers
“Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the AEDC 16T propulsion wind tunnel” Metadata:
- Title: ➤ Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the AEDC 16T propulsion wind tunnel
- Author: Paul M. Siemers
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1986
- Publish Location: Hampton, Va
“Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the AEDC 16T propulsion wind tunnel” Subjects and Themes:
- Subjects: ➤ Aerodynamic load - Forebodies - Pressure distribution - Space shuttle orbiters - Space shuttles - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17727214M
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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34Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the Ames unitary plan wind tunnel
By Paul M. Siemers
“Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the Ames unitary plan wind tunnel” Metadata:
- Title: ➤ Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the Ames unitary plan wind tunnel
- Author: Paul M. Siemers
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1986
- Publish Location: Hampton, Va
“Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the Ames unitary plan wind tunnel” Subjects and Themes:
- Subjects: ➤ Space shuttles - Pressure distribution - Aerodynamic load - Models - Forebodies - Wind tunnel tests - Orifices
Edition Identifiers:
- The Open Library ID: OL17727215M
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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35Transonic airfoil design on the Navier-Stokes equations to attain arbitrarily specified pressure distribution - an iterative procedure
By Naoki Hirose
“Transonic airfoil design on the Navier-Stokes equations to attain arbitrarily specified pressure distribution - an iterative procedure” Metadata:
- Title: ➤ Transonic airfoil design on the Navier-Stokes equations to attain arbitrarily specified pressure distribution - an iterative procedure
- Author: Naoki Hirose
- Number of Pages: Median: 16
- Publisher: National Aerospace Laboratory
- Publish Date: 1986
- Publish Location: Chofu, Tokyo, Japan
“Transonic airfoil design on the Navier-Stokes equations to attain arbitrarily specified pressure distribution - an iterative procedure” Subjects and Themes:
- Subjects: Pressure distribution - Airfoils - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL20984570M
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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36Approximate calculation of the pressure distribution on a rectangular wing oscillating in incompressible flow
By E. D. Poppleton
“Approximate calculation of the pressure distribution on a rectangular wing oscillating in incompressible flow” Metadata:
- Title: ➤ Approximate calculation of the pressure distribution on a rectangular wing oscillating in incompressible flow
- Author: E. D. Poppleton
- Number of Pages: Median: 26
- Publisher: Institute of Aerophysics
- Publish Date: 1958
- Publish Location: [Downsview, Ont.]
“Approximate calculation of the pressure distribution on a rectangular wing oscillating in incompressible flow” Subjects and Themes:
- Subjects: Pressure distribution - Unsteady flow - Flutter - Wings
Edition Identifiers:
- The Open Library ID: OL19251806M
Access and General Info:
- First Year Published: 1958
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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37Heat transfer and flow on the first stage blade tip of a power generation gas turbine
By Ronald S. Bunker
“Heat transfer and flow on the first stage blade tip of a power generation gas turbine” Metadata:
- Title: ➤ Heat transfer and flow on the first stage blade tip of a power generation gas turbine
- Author: Ronald S. Bunker
- 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]
“Heat transfer and flow on the first stage blade tip of a power generation gas turbine” Subjects and Themes:
- Subjects: ➤ Gas turbines - Heat transfer - Convective heat transfer - Blade tips - Pressure distribution - Heat transfer coefficients - Turbine blades
Edition Identifiers:
- The Open Library ID: OL15552406M
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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38Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds
By Patsy S. Fulton
“Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds” Metadata:
- Title: ➤ Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds
- Author: Patsy S. Fulton
- Language: English
- Number of Pages: Median: 115
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1988
- Publish Location: Hampton, Va - [Springfield, Va
“Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds” Subjects and Themes:
- Subjects: ➤ Guided missiles - Aerodynamics - Supersonic flow - Angle of attack - Pressure distribution - Transonic flow - Wind tunnel models - Euler equations of motion - Wind tunnel tests - Missile configurations
Edition Identifiers:
- The Open Library ID: OL15407176M
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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39Pressures inside a room subjected to sonic boom
By Nabil Naguib Wahba
“Pressures inside a room subjected to sonic boom” Metadata:
- Title: ➤ Pressures inside a room subjected to sonic boom
- Author: Nabil Naguib Wahba
- Publisher: ➤ Institute for Aerospace Studies
- Publish Date: 1977
- Publish Location: [Downsview, Ont.]
“Pressures inside a room subjected to sonic boom” Subjects and Themes:
- Subjects: Pressure distribution - Sonic booms
Edition Identifiers:
- The Open Library ID: OL20899527M
Access and General Info:
- First Year Published: 1977
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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40Handbook of inviscid sphere-cone flow fields and pressure distributions. Volume 1
By A. M. Morrison
“Handbook of inviscid sphere-cone flow fields and pressure distributions. Volume 1” Metadata:
- Title: ➤ Handbook of inviscid sphere-cone flow fields and pressure distributions. Volume 1
- Author: A. M. Morrison
- Number of Pages: Median: 554
- Publisher: Naval Surface Weapons Center
- Publish Date: 1975
- Publish Location: Silver Spring, Md
“Handbook of inviscid sphere-cone flow fields and pressure distributions. Volume 1” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL19047093M
Access and General Info:
- First Year Published: 1975
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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41Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system
By J. R. DeBonis
“Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system” Metadata:
- Title: ➤ Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system
- Author: J. R. DeBonis
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - Available from NASA Center for Aerospace Information
- Publish Date: 2001
- Publish Location: ➤ Hanover, MD - [Cleveland, Ohio]
“Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Air breathing boosters - Pressure distribution - Propulsion - Wind tunnel tests - Hypersonic speed
Edition Identifiers:
- The Open Library ID: OL16028849M
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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42Experimental optimization methods for multi-element airfoils
By Drew Landman
“Experimental optimization methods for multi-element airfoils” Metadata:
- Title: ➤ Experimental optimization methods for multi-element airfoils
- Author: Drew Landman
- Language: English
- Publisher: ➤ Dept. of Mechanical Engineering, College of Engineering & Technology, Old Dominion University - National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1996
- Publish Location: ➤ Norfolk, Va - [Washington, DC - Springfield, Va
“Experimental optimization methods for multi-element airfoils” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Reynolds number - Angle of attack - Pressure distribution - Flaps (Control surfaces) - Optimization - Airfoils - Computer programs
Edition Identifiers:
- The Open Library ID: OL15506398M
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:
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43Rapid numerical simulation of viscous axisymmetric flow fields
By Daniel L. Tweedt
“Rapid numerical simulation of viscous axisymmetric flow fields” Metadata:
- Title: ➤ Rapid numerical simulation of viscous axisymmetric flow fields
- Author: Daniel L. Tweedt
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Rapid numerical simulation of viscous axisymmetric flow fields” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Viscous flow - Axisymmetric flow - Pressure distribution - Transonic flow - Turbulence models - Finite difference theory - Navier-Stokes equation - Flow distribution - Runge-Kutta method - Shock waves
Edition Identifiers:
- The Open Library ID: OL15420864M
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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44Analysis of advanced solid rocket motor ignition phenomena
By Winfred A. Foster
“Analysis of advanced solid rocket motor ignition phenomena” Metadata:
- Title: ➤ Analysis of advanced solid rocket motor ignition phenomena
- Author: Winfred A. Foster
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Analysis of advanced solid rocket motor ignition phenomena” Subjects and Themes:
- Subjects: ➤ Solid propellant rocket engines - Pressure distribution - Heat transfer coefficients - Wind tunnel tests - Scale models - Propulsion system performance - Advanced solid rocket motor (STS) - Flow distribution - Ignition - Space shuttle boosters
Edition Identifiers:
- The Open Library ID: OL15418933M
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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45Performance and pressure data from a small model tilt-rotor in hover
By Lonnie Branum
“Performance and pressure data from a small model tilt-rotor in hover” Metadata:
- Title: ➤ Performance and pressure data from a small model tilt-rotor in hover
- Author: Lonnie Branum
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - Moffett Field, CA
“Performance and pressure data from a small model tilt-rotor in hover” Subjects and Themes:
- Subjects: Tilting rotors - Pressure measurement - Hovering - Pressure distribution - Tilt rotor aircraft
Edition Identifiers:
- The Open Library ID: OL15500640M
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:
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46Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds
By Elizabeth B. Plentovich
“Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds” Metadata:
- Title: ➤ Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds
- Author: Elizabeth B. Plentovich
- Language: English
- Number of Pages: Median: 51
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1991
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds” Subjects and Themes:
- Subjects: ➤ Aerodynamic load - Aerodynamics, Transonic - Cavities - Cavities (Airplanes) - Flow distribution - High Reynolds number - Mach number - Pressure distribution - Reynolds number - Subsonic flow - Transonic Aerodynamics - Transonic flow - Turbulent boundary layer - Yaw - Yawing (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL16135213M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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47Numerical analysis of base flowfield for a four-engine clustered nozzle configuration
By Ten-See Wang
“Numerical analysis of base flowfield for a four-engine clustered nozzle configuration” Metadata:
- Title: ➤ Numerical analysis of base flowfield for a four-engine clustered nozzle configuration
- Author: Ten-See Wang
- Language: English
- Publisher: ➤ [National Aeronautics and Space Administration - National Technical Information Service, distributor - American Institute of Aeronautics and Astronautics
- Publish Date: 1995
- Publish Location: ➤ Washington, DC - Springfield, Va
“Numerical analysis of base flowfield for a four-engine clustered nozzle configuration” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Base flow - Turbulent flow - Pressure distribution - Flow distribution - Grid generation (Mathematics) - Multiengine vehicles - Nozzle flow - Base pressure
Edition Identifiers:
- The Open Library ID: OL15542985M
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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48Study of the kinematic and load sharing properties of wormgearing with non-symmetric tooth profiles
By D. C. Sun
“Study of the kinematic and load sharing properties of wormgearing with non-symmetric tooth profiles” Metadata:
- Title: ➤ Study of the kinematic and load sharing properties of wormgearing with non-symmetric tooth profiles
- Author: D. C. Sun
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Study of the kinematic and load sharing properties of wormgearing with non-symmetric tooth profiles” Subjects and Themes:
- Subjects: ➤ Transmissions (Machine elements) - Helicopter propeller drive - Gear teeth - Hydrostatic pressure - Pressure distribution - Kinematics
Edition Identifiers:
- The Open Library ID: OL15411780M
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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49Interaction of sound from supersonic jets with nearby structures
By C. C. Fenno
“Interaction of sound from supersonic jets with nearby structures” Metadata:
- Title: ➤ Interaction of sound from supersonic jets with nearby structures
- Author: C. C. Fenno
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Institute for Computer Applications in Science and Engineering, NASA Langley Research Center
- Publish Date: 1997
- Publish Location: [Springfield, Va - Hampton, VA
“Interaction of sound from supersonic jets with nearby structures” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Velocity distribution - Aircraft structures - Aeroacoustics - Interactions - Pressure distribution - Supersonic jet flow
Edition Identifiers:
- The Open Library ID: OL15505132M
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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50Aerothermal tests of spherical dome protuberances on a flat plate at a Mach number of 6.5
By Christopher E. Glass
“Aerothermal tests of spherical dome protuberances on a flat plate at a Mach number of 6.5” Metadata:
- Title: ➤ Aerothermal tests of spherical dome protuberances on a flat plate at a Mach number of 6.5
- Author: Christopher E. Glass
- Number of Pages: Median: 58
- Publisher: Langley Research Center
- Publish Date: 1986
- Publish Location: Hampton, Va
“Aerothermal tests of spherical dome protuberances on a flat plate at a Mach number of 6.5” Subjects and Themes:
- Subjects: ➤ Laminar boundary layer - Turbulent boundary layer - Thermal protection - Hypersonic aircraft - Pressure distribution - Protuberances
Edition Identifiers:
- The Open Library ID: OL20985986M
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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