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Source: The Open Library
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1Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack
By Brent R. Cobleigh
“Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack” Metadata:
- Title: ➤ Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack
- Author: Brent R. Cobleigh
- Language: English
- Publisher: ➤ Available from NASA Center for AeroSpace Information (CASI) - National Aeronautics and Space Administration, Dryden Flight Research Center
- Publish Date: 2001
- Publish Location: Edwards, Calif - Hanover, MD
“Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack” Subjects and Themes:
- Subjects: ➤ Asymmetry - Flight envelopes - Forebodies - Water tunnel tests - Wind tunnel tests - Yawing moments
Edition Identifiers:
- The Open Library ID: OL18170318M - OL18767809M - OL17615296M - OL17718695M
- Online Computer Library Center (OCLC) ID: 52130350
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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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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2Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model
By Stacey J. Cotton
“Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model” Metadata:
- Title: ➤ Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model
- Author: Stacey J. Cotton
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Angle of attack - Buffeting - Flight tests - Flow visualization - Liquid-vapor interfaces - Scale models - Sideslip - Stabilizers (Fluid dynamics) - Tail assemblies - Vortices - Water tunnel tests - X-29 aircraft
Edition Identifiers:
- The Open Library ID: OL17001977M - OL17682958M - OL18076527M
- Online Computer Library Center (OCLC) ID: 32298726
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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3Delta wing vortex manipulation using pulsed and steady blowing during ramp pitching
By J. Moreira
“Delta wing vortex manipulation using pulsed and steady blowing during ramp pitching” Metadata:
- Title: ➤ Delta wing vortex manipulation using pulsed and steady blowing during ramp pitching
- Author: J. Moreira
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - Mechanical Engineering Dept., Worcester Polytechnic Institute - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC - Springfield, Va - Worcester, MA
“Delta wing vortex manipulation using pulsed and steady blowing during ramp pitching” Subjects and Themes:
- Subjects: Angle of attack - Delta wings - Spanwise blowing - Vortex breakdown - Water tunnel tests
Edition Identifiers:
- The Open Library ID: OL15419012M - OL17793986M
- Online Computer Library Center (OCLC) ID: 34612627
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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4Simultaneous three-dimensional velocity and mixing measurements by use of laser Doppler velocimetry and fluorescence probes in a water tunnel
By Dan H. Neuhart
“Simultaneous three-dimensional velocity and mixing measurements by use of laser Doppler velocimetry and fluorescence probes in a water tunnel” Metadata:
- Title: ➤ Simultaneous three-dimensional velocity and mixing measurements by use of laser Doppler velocimetry and fluorescence probes in a water tunnel
- Author: Dan H. Neuhart
- Language: English
- Number of Pages: Median: 84
- Publisher: ➤ Lewis Research Center - National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: Hampton, Va - [Springfield, Va
“Simultaneous three-dimensional velocity and mixing measurements by use of laser Doppler velocimetry and fluorescence probes in a water tunnel” Subjects and Themes:
- Subjects: Laser velocimeters - Water tunnel tests
Edition Identifiers:
- The Open Library ID: OL16982133M - OL19754416M
- Online Computer Library Center (OCLC) ID: 32145509
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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5Simultaneous three-dimensional velocity and mixing measurments by use of laser Doppler velocimetry and fluorescence probes in a water tunnel
By Dan H. Neuhart
“Simultaneous three-dimensional velocity and mixing measurments by use of laser Doppler velocimetry and fluorescence probes in a water tunnel” Metadata:
- Title: ➤ Simultaneous three-dimensional velocity and mixing measurments by use of laser Doppler velocimetry and fluorescence probes in a water tunnel
- Author: Dan H. Neuhart
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: Hampton, Va - [Springfield, Va
“Simultaneous three-dimensional velocity and mixing measurments by use of laser Doppler velocimetry and fluorescence probes in a water tunnel” Subjects and Themes:
- Subjects: ➤ Velocity distribution - Laser Doppler velocimeters - Flow velocity - Fluorescence - Jet flow - Flow meaurement - Vortices - Nonintrusive measurement - Water - Velocity measurement - Flow visualization - Dyes - Water tunnel tests
Edition Identifiers:
- The Open Library ID: OL18075782M - OL15402596M
Access and General Info:
- First Year Published: 1994
- 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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6New flow visualization technique for water tunnel testing of combustors
By Joseph A. Schetz
“New flow visualization technique for water tunnel testing of combustors” Metadata:
- Title: ➤ New flow visualization technique for water tunnel testing of combustors
- Author: Joseph A. Schetz
- Number of Pages: Median: 46
- Publisher: ➤ Aero Propulsion Laboratory, Air Force Wright Aeronautical Laboratories
- Publish Date: 1985
- Publish Location: ➤ Wright Patterson Air Force Base, Ohio
“New flow visualization technique for water tunnel testing of combustors” Subjects and Themes:
- Subjects: Combustion chambers - Flow visualization - Water tunnel tests
Edition Identifiers:
- The Open Library ID: OL19985990M
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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7Development of a multicomponent force and moment balance for water tunnel applications
By Carlos J. Suarez
“Development of a multicomponent force and moment balance for water tunnel applications” Metadata:
- Title: ➤ Development of a multicomponent force and moment balance for water tunnel applications
- Author: Carlos J. Suarez
- Publisher: NASA
- Publish Date: 1994
- Publish Location: Washington, D. C
“Development of a multicomponent force and moment balance for water tunnel applications” Subjects and Themes:
- Subjects: Water tunnel tests
Edition Identifiers:
- The Open Library ID: OL21369363M
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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8An investigation of the quantitative applicability of model helicopter rotor wake patterns obtained from a water tunnel
By Anton J. Landgrebe
“An investigation of the quantitative applicability of model helicopter rotor wake patterns obtained from a water tunnel” Metadata:
- Title: ➤ An investigation of the quantitative applicability of model helicopter rotor wake patterns obtained from a water tunnel
- Author: Anton J. Landgrebe
- Number of Pages: Median: 123
- Publisher: ➤ United Aircraft Corporation Research Laboratories
- Publish Date: 1971
- Publish Location: East Hartford, Conn
“An investigation of the quantitative applicability of model helicopter rotor wake patterns obtained from a water tunnel” Subjects and Themes:
- Subjects: Helicopter wakes - Rotors - Water tunnel tests
Edition Identifiers:
- The Open Library ID: OL19245856M
Access and General Info:
- First Year Published: 1971
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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9Water tunnel flow visualization study through poststall of 12 novel planform shapes
By Gregory M. Gatlin
“Water tunnel flow visualization study through poststall of 12 novel planform shapes” Metadata:
- Title: ➤ Water tunnel flow visualization study through poststall of 12 novel planform shapes
- Author: Gregory M. Gatlin
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: Hampton, Va - [Springfield, Va
“Water tunnel flow visualization study through poststall of 12 novel planform shapes” Subjects and Themes:
- Subjects: ➤ Planforms - Water tunnel tests - Flow visualization - Aerodynamic configurations - Free flow - Wing profiles - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15503578M
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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10Water tunnel flow visualization study of a 4.4% scale X-31 forebody
By Brent R. Cobleigh
“Water tunnel flow visualization study of a 4.4% scale X-31 forebody” Metadata:
- Title: ➤ Water tunnel flow visualization study of a 4.4% scale X-31 forebody
- Author: Brent R. Cobleigh
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility
- Publish Date: 1994
- Publish Location: ➤ Edwards, Calif - [Springfield, Va
“Water tunnel flow visualization study of a 4.4% scale X-31 forebody” Subjects and Themes:
- Subjects: ➤ X-31 aircraft - Strakes - Vortices - Forebodies - Angle of attack - Asymmetry - Flow visualization - Water tunnel tests
Edition Identifiers:
- The Open Library ID: OL15403687M
Access and General Info:
- First Year Published: 1994
- 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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11Feasibility of generating an "artificial" burst in a turbulent boundary layer
By M. Gad-el-Hak
“Feasibility of generating an "artificial" burst in a turbulent boundary layer” Metadata:
- Title: ➤ Feasibility of generating an "artificial" burst in a turbulent boundary layer
- Author: M. Gad-el-Hak
- Language: English
- Number of Pages: Median: 50
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1986
- Publish Location: [Washington, D.C.]
“Feasibility of generating an "artificial" burst in a turbulent boundary layer” Subjects and Themes:
- Subjects: ➤ Turbulent boundary layer - Mathematical models - Drag reduction - Vortex generators - Laminar flow - Bursts - Water tunnel tests - Vortices
Edition Identifiers:
- The Open Library ID: OL16122036M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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12Visualisation in water of vortex flow over sharp-edged canard configurations
By D. H. Thompson
“Visualisation in water of vortex flow over sharp-edged canard configurations” Metadata:
- Title: ➤ Visualisation in water of vortex flow over sharp-edged canard configurations
- Author: D. H. Thompson
- Number of Pages: Median: 40
- Publisher: ➤ Australia, Dept. of Defence, Aeronautical Research Laboratory
- Publish Date: 1992
- Publish Location: Melbourne, Victoria
“Visualisation in water of vortex flow over sharp-edged canard configurations” Subjects and Themes:
- Subjects: Canard configurations - Water tunnel tests - Flow visualization - Vortices
Edition Identifiers:
- The Open Library ID: OL19245372M
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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13Water tunnel flow visualisation of vortex breakdown over the F/A-18
By D. H. Thompson
“Water tunnel flow visualisation of vortex breakdown over the F/A-18” Metadata:
- Title: ➤ Water tunnel flow visualisation of vortex breakdown over the F/A-18
- Author: D. H. Thompson
- Number of Pages: Median: 43
- Publisher: ➤ Aeronautical Research Laboratory
- Publish Date: 1990
- Publish Location: Melbourne, Victoria
“Water tunnel flow visualisation of vortex breakdown over the F/A-18” Subjects and Themes:
- Subjects: Water tunnel tests - Vortex breakdown - Flow visualization
Edition Identifiers:
- The Open Library ID: OL19165566M
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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