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Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Study of optical techniques for the Ames unitary wind tunnels
By Lee, George.
“Study of optical techniques for the Ames unitary wind tunnels” Metadata:
- Title: ➤ Study of optical techniques for the Ames unitary wind tunnels
- Author: Lee, George.
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - MCAT Institute - National Aeronautics and Space Administration
- Publish Date: 1992 - 1993
- Publish Location: ➤ [Springfield, Va - [Springfield, Va.? - Springfield, Va - San Jose, CA - [Washington, D.C
“Study of optical techniques for the Ames unitary wind tunnels” Subjects and Themes:
- Subjects: Wind tunnels
Edition Identifiers:
- The Open Library ID: ➤ OL17681106M - OL14704069M - OL17681107M - OL17676520M - OL14685876M - OL17786415M - OL17751776M - OL17678380M - OL17675296M - OL17676729M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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2Recommended Practice
By American Institute of Aeronautics and As

“Recommended Practice” Metadata:
- Title: Recommended Practice
- Author: ➤ American Institute of Aeronautics and As
- Language: English
- Number of Pages: Median: 74
- Publisher: ➤ AIAA (American Institute of Aeronautics & Ast
- Publish Date: 2002 - 2003 - 2004
“Recommended Practice” Subjects and Themes:
- Subjects: ➤ Wind tunnels - Standards - Strain gages - Calibration - Aerodynamics - Research - Wind tunnel models - Testing - Drone aircraft - Terminology
Edition Identifiers:
- The Open Library ID: ➤ OL8644127M - OL12135805M - OL12135810M - OL12135806M - OL12135824M - OL8644125M - OL9800190M - OL12135809M - OL8644126M
- Online Computer Library Center (OCLC) ID: 50554216 - 53330774 - 53002601 - 52520442 - 54865685
- Library of Congress Control Number (LCCN): 2003014347 - 2004005431 - 2003023502
- All ISBNs: ➤ 9781563476518 - 1563476614 - 9781563476532 - 9781563476457 - 1563476622 - 9781563476464 - 1563476460 - 1563475596 - 1563476525 - 1563476452 - 9781563476617 - 9781563476624 - 9781563476525 - 1563476517 - 9781563475597 - 1563477076 - 1563476533 - 9781563477072
Access and General Info:
- First Year Published: 2002
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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3Hot-jet simulation in cryogenic wind tunnels
By Keisuke Asai
“Hot-jet simulation in cryogenic wind tunnels” Metadata:
- Title: ➤ Hot-jet simulation in cryogenic wind tunnels
- Author: Keisuke Asai
- Language: English
- Number of Pages: Median: 45
- Publisher: ➤ For sale by the National Technical Information Service] - Langley Research Center - National Aeronautics and SpaceAdministration - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
- Publish Date: 1989
- Publish Location: ➤ Washington D.C - Hampton, Va - Washington, D.C - [Springfield, Va - [Washington, DC]
“Hot-jet simulation in cryogenic wind tunnels” Subjects and Themes:
- Subjects: ➤ Cryogenic wind tunnels - Exhaust flow simulation - Jet flow - Reynolds number - Wind tunnel tests - Wind tunnels
Edition Identifiers:
- The Open Library ID: ➤ OL17683287M - OL19959189M - OL13931490M - OL15576426M - OL18208937M - OL19379736M - OL18078046M - OL1812959M
- Online Computer Library Center (OCLC) ID: 20034307
- Library of Congress Control Number (LCCN): 89602567
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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4Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing
By Thomas A. Byrdsong
“Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing” Metadata:
- Title: ➤ Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing
- Author: Thomas A. Byrdsong
- Language: English
- Number of Pages: Median: 211
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
- Publish Date: 1983
- Publish Location: ➤ [Springfield, Va - Washington, D.C
“Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing” Subjects and Themes:
- Subjects: Wind tunnels - Airplanes - Wings - Aerodynamic load
Edition Identifiers:
- The Open Library ID: ➤ OL15304178M - OL17125863M - OL18036363M - OL17125861M - OL18036359M - OL17076680M - OL17076678M
Access and General Info:
- First Year Published: 1983
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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5Wind-tunnel pressure data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊
By Emma Jean Landrum
“Wind-tunnel pressure data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊” Metadata:
- Title: ➤ Wind-tunnel pressure data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊
- Author: Emma Jean Landrum
- Language: English
- Number of Pages: Median: 149
- Publisher: ➤ for sale by the National Technical Information Service - National Aeronautics and Space Administration
- Publish Date: 1977
- Publish Location: ➤ Washington, DC - Springfield, Va - Washington
“Wind-tunnel pressure data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊” Subjects and Themes:
- Subjects: ➤ Body of revolution - Control systems - Flow visualization - Guided missiles - Measurement - Pressure - Wind tunnels
Edition Identifiers:
- The Open Library ID: ➤ OL18012850M - OL17977702M - OL13841150M - OL17117393M - OL14927270M - OL15219004M
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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6Langley 8-ft. HTT test 139 gas analyses
By Danny R. Sprinkle
“Langley 8-ft. HTT test 139 gas analyses” Metadata:
- Title: ➤ Langley 8-ft. HTT test 139 gas analyses
- Author: Danny R. Sprinkle
- Language: English
- Number of Pages: Median: 192
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1999
- Publish Location: Hampton, Va - [Springfield, Va
“Langley 8-ft. HTT test 139 gas analyses” Subjects and Themes:
- Subjects: ➤ Hypersonic wind tunnels - Mass spectroscopy - Gas analysis - Blowdown wind tunnels - Wind tunnel calibration - Wind tunnels - Gases - Analysis
Edition Identifiers:
- The Open Library ID: ➤ OL15563082M - OL17593827M - OL17137902M - OL18139210M - OL17138164M - OL20327205M
- Online Computer Library Center (OCLC) ID: 43627661
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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7KC-135 Winglet Program Review
By KC-135 Winglet Program Review (1981 Edwards, Calif.)
“KC-135 Winglet Program Review” Metadata:
- Title: KC-135 Winglet Program Review
- Author: ➤ KC-135 Winglet Program Review (1981 Edwards, Calif.)
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1982
- Publish Location: [Washington, D.C.?]
“KC-135 Winglet Program Review” Subjects and Themes:
- Subjects: Wind tunnels - Airplanes - Wings - Aerofoils
Edition Identifiers:
- The Open Library ID: ➤ OL15320030M - OL18040928M - OL17558249M - OL14931689M - OL17978922M - OL17081277M
Access and General Info:
- First Year Published: 1982
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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8Wind Tunnel Testing of High-Rise Buildings
By Peter Irwin
“Wind Tunnel Testing of High-Rise Buildings” Metadata:
- Title: ➤ Wind Tunnel Testing of High-Rise Buildings
- Author: Peter Irwin
- Language: English
- Publisher: ➤ Routledge - Taylor & Francis Group - CRC Press LLC
- Publish Date: 2013 - 2019
“Wind Tunnel Testing of High-Rise Buildings” Subjects and Themes:
- Subjects: ➤ Tall buildings - Wind tunnels - Structural analysis (engineering)
Edition Identifiers:
- The Open Library ID: ➤ OL46033161M - OL39255306M - OL39242708M - OL36236848M - OL36209422M - OL34658469M
- All ISBNs: ➤ 1138470430 - 9781317999959 - 9781317999942 - 1315879522 - 9781317999966 - 1317999967 - 9781299685994 - 9781315879529 - 9781138470439 - 1317999959 - 1317999940 - 1299685994
Access and General Info:
- First Year Published: 2013
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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9Wind-tunnel testing
By Alan Pope
“Wind-tunnel testing” Metadata:
- Title: Wind-tunnel testing
- Author: Alan Pope
- Language: English
- Number of Pages: Median: 511
- Publisher: ➤ Chapman and Hall - Wiley - WILEY, JOHN @ & SONS
- Publish Date: 1947 - 1954
- Publish Location: New York - London
“Wind-tunnel testing” Subjects and Themes:
- Subjects: Aeroplanes - Models - Testing - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL47029906M - OL13952347M - OL20658547M - OL42957362M - OL20877235M
Access and General Info:
- First Year Published: 1947
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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10Wind-tunnel force and flow visualization data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊
By Emma Jean Landrum
“Wind-tunnel force and flow visualization data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊” Metadata:
- Title: ➤ Wind-tunnel force and flow visualization data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊
- Author: Emma Jean Landrum
- Language: English
- Number of Pages: Median: 149
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1979
- Publish Location: ➤ [Springfield, Va - Washington, D.C
“Wind-tunnel force and flow visualization data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊” Subjects and Themes:
- Subjects: Aerodynamics - Wind tunnels - Body of revolution - Flow visualization
Edition Identifiers:
- The Open Library ID: OL14925560M - OL17122624M - OL18021717M - OL17977161M - OL15255679M
Access and General Info:
- First Year Published: 1979
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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11Evaluation of wind-tunnel gust response technique correlations with analytical and flight test results
By L. Tracy Redd
“Evaluation of wind-tunnel gust response technique correlations with analytical and flight test results” Metadata:
- Title: ➤ Evaluation of wind-tunnel gust response technique correlations with analytical and flight test results
- Author: L. Tracy Redd
- Language: English
- Number of Pages: Median: 52
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
- Publish Date: 1979
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“Evaluation of wind-tunnel gust response technique correlations with analytical and flight test results” Subjects and Themes:
- Subjects: Wind tunnels - Atmospheric turbulence - Frequency response (Dynamics)
Edition Identifiers:
- The Open Library ID: OL15263207M - OL18024169M - OL17549922M - OL14932452M - OL17979246M
Access and General Info:
- First Year Published: 1979
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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12Wind-tunnel testing
By Pope, Alan
“Wind-tunnel testing” Metadata:
- Title: Wind-tunnel testing
- Author: Pope, Alan
- Language: English
- Number of Pages: Median: 511
- Publisher: J. Wiley - Wiley
- Publish Date: 1947 - 1954
- Publish Location: New York
“Wind-tunnel testing” Subjects and Themes:
- Subjects: Airplanes - Models - Testing - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL6523015M - OL17356212M - OL21233365M - OL6155004M - OL17461127M
- Online Computer Library Center (OCLC) ID: 2559067
- Library of Congress Control Number (LCCN): 47031381 - 54008525
Access and General Info:
- First Year Published: 1947
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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13The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel
By Paul T. Soderman
“The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel” Metadata:
- Title: ➤ The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel
- Author: Paul T. Soderman
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1992
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va
“The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel” Subjects and Themes:
- Subjects: Wind tunnels
Edition Identifiers:
- The Open Library ID: OL15365188M - OL17106573M - OL16949017M - OL18054925M
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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14Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel
By P. S. Barna
“Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel” Metadata:
- Title: ➤ Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel
- Author: P. S. Barna
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995 - 1996
- Publish Location: Hampton, Va - [Springfield, Va
“Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel” Subjects and Themes:
- Subjects: ➤ Acoustic ducts - Blowing - Diffusers - Flow visualization - Nozzle design - Pressure recovery - Scale models - Sound detecting and ranging - Sound waves - Three dimensional models - Velocity measurement - Wind tunnel models - Wind tunnel nozzles - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL17838013M - OL15504898M - OL15504897M - OL17838014M
- Online Computer Library Center (OCLC) ID: 40132872 - 40122403
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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15Wind-tunnel test of an articulated helicopter rotor model with several tip shapes
By John D. Berry
“Wind-tunnel test of an articulated helicopter rotor model with several tip shapes” Metadata:
- Title: ➤ Wind-tunnel test of an articulated helicopter rotor model with several tip shapes
- Author: John D. Berry
- Language: English
- Number of Pages: Median: 92
- Publisher: ➤ Fo r sale by the National Technical Information Service] - National Aeronautics and Space Administrat ion, Scientific and Technical Information Branch
- Publish Date: 1980
- Publish Location: ➤ [Springfield, Va - Washington, D.C
“Wind-tunnel test of an articulated helicopter rotor model with several tip shapes” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Ground simulators - Helicopters - Rotors (Helicopters) - Testing - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL18018933M - OL17070621M - OL15246496M - OL17121249M
Access and General Info:
- First Year Published: 1980
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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16Aeronautical facilities catalogue
By Frank E. Peñaranda
“Aeronautical facilities catalogue” Metadata:
- Title: ➤ Aeronautical facilities catalogue
- Author: Frank E. Peñaranda
- Language: English
- Publisher: ➤ Scientific and Technical Information Branch, National Aeronautics and Space Administration - For sale by the National Technical Information Service] - For sale by the National Aeronautics and Space Administration] - For sale by the Supt. of Docs., U.S. G.P.O.]
- Publish Date: 1985 - 1986
- Publish Location: ➤ Washington, DC - [Springfield, Va
“Aeronautical facilities catalogue” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Aeronautics - Catalogs - Flight simulators - Hypersonic wind tunnels - Research - Supersonic wind tunnels - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL17658875M - OL17832292M - OL17667072M - OL2664364M
- Library of Congress Control Number (LCCN): 85601812
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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17Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing
By Thomas A Byrdsong
“Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing” Metadata:
- Title: ➤ Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing
- Author: Thomas A Byrdsong
- Language: English
- Number of Pages: Median: 193
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1983
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing” Subjects and Themes:
- Subjects: Wind tunnels - Airplanes - Wings - Aerodynamic load
Edition Identifiers:
- The Open Library ID: OL17977369M - OL14926213M - OL16806751M - OL17977366M
Access and General Info:
- First Year Published: 1983
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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18Finite-rate water condensation in combustion-heated wind tunnels
By Wayne D. Erickson
“Finite-rate water condensation in combustion-heated wind tunnels” Metadata:
- Title: ➤ Finite-rate water condensation in combustion-heated wind tunnels
- Author: Wayne D. Erickson
- Language: English
- Number of Pages: Median: 69
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service - Langley Research Center
- Publish Date: 1988
- Publish Location: ➤ [Washington, D.C.] - Springfield, Va - Hampton, Va
“Finite-rate water condensation in combustion-heated wind tunnels” Subjects and Themes:
- Subjects: ➤ Condensation - Nucleation - Combustion wind tunnels - Wind tunnels - High temperature environments - Condensing - Measurement - Combustion products - Water - Droplet growth
Edition Identifiers:
- The Open Library ID: OL18926475M - OL17724286M - OL18468583M - OL18217728M
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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19Aero-thermal calibration of the NASA Glenn icing research tunnel (2000 tests)
By Jose C. Gonsalez
“Aero-thermal calibration of the NASA Glenn icing research tunnel (2000 tests)” Metadata:
- Title: ➤ Aero-thermal calibration of the NASA Glenn icing research tunnel (2000 tests)
- Author: Jose C. Gonsalez
- Language: English
- Number of Pages: Median: 39
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2001
- Publish Location: ➤ [Cleveland, Ohio] - Hanover, MD
“Aero-thermal calibration of the NASA Glenn icing research tunnel (2000 tests)” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Wind tunnels - Icing (Meteorology) - Icing - Calibration - Subsonic - Wind tunnel - Flow quality
Edition Identifiers:
- The Open Library ID: OL17720603M - OL17621382M - OL18902555M - OL18184182M
- Online Computer Library Center (OCLC) ID: 51020691
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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20Flight and wind-tunnel calibrations of a flush airdata sensor at high angles of attack and sideslip and at supersonic mach numbers
By Timothy R. Moes
“Flight and wind-tunnel calibrations of a flush airdata sensor at high angles of attack and sideslip and at supersonic mach numbers” Metadata:
- Title: ➤ Flight and wind-tunnel calibrations of a flush airdata sensor at high angles of attack and sideslip and at supersonic mach numbers
- Author: Timothy R. Moes
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Dryden Flight Research Facility - National Technical Information Service, [distributor]
- Publish Date: 1993
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“Flight and wind-tunnel calibrations of a flush airdata sensor at high angles of attack and sideslip and at supersonic mach numbers” Subjects and Themes:
- Subjects: Wind tunnels - Detectors
Edition Identifiers:
- The Open Library ID: OL18059906M - OL14694022M - OL15375539M - OL17109033M
Access and General Info:
- First Year Published: 1993
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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21X-29A longitudinal and directional force and moment supplemental transonic wind tunnel test results
By Albion H. Bowers
“X-29A longitudinal and directional force and moment supplemental transonic wind tunnel test results” Metadata:
- Title: ➤ X-29A longitudinal and directional force and moment supplemental transonic wind tunnel test results
- Author: Albion H. Bowers
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration,Ames Research Center, Dryden Flight Research Facility - For sale by the National Technical Information Service
- Publish Date: 1984
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“X-29A longitudinal and directional force and moment supplemental transonic wind tunnel test results” Subjects and Themes:
- Subjects: Aerodynamics - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL14662657M - OL15273671M - OL18028405M - OL17095319M
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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22On-line analysis capabilities developed to support the AFW wind-tunnel tests
By Carol D. Wieseman
“On-line analysis capabilities developed to support the AFW wind-tunnel tests” Metadata:
- Title: ➤ On-line analysis capabilities developed to support the AFW wind-tunnel tests
- Author: Carol D. Wieseman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - For sale by the National Technical Information Service
- Publish Date: 1992
- Publish Location: Hampton, Va - [Springfield, Va
“On-line analysis capabilities developed to support the AFW wind-tunnel tests” Subjects and Themes:
- Subjects: Wind tunnels - Testing
Edition Identifiers:
- The Open Library ID: OL18055410M - OL17106898M - OL17676493M - OL16952706M
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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23Validation of vortex-lattice method for loads on wings in lift-generated wakes
By Vernon J. Rossow
“Validation of vortex-lattice method for loads on wings in lift-generated wakes” Metadata:
- Title: ➤ Validation of vortex-lattice method for loads on wings in lift-generated wakes
- Author: Vernon J. Rossow
- Language: English
- Publisher: ➤ American Institute of Aeronautics and Astronautics - [National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - Washington, DC
“Validation of vortex-lattice method for loads on wings in lift-generated wakes” Subjects and Themes:
- Subjects: ➤ Force distribution - Lift - Loads (Forces) - Rolling moments - Subsonic speed - Vortex lattice method - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL17594006M - OL15507839M - OL17126890M - OL18122121M
- Online Computer Library Center (OCLC) ID: 40348464
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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24NASA Lewis 9-by 15-foot low-speed wind tunnel user manual
By Ronald H. Soeder
“NASA Lewis 9-by 15-foot low-speed wind tunnel user manual” Metadata:
- Title: ➤ NASA Lewis 9-by 15-foot low-speed wind tunnel user manual
- Author: Ronald H. Soeder
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1993
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“NASA Lewis 9-by 15-foot low-speed wind tunnel user manual” Subjects and Themes:
- Subjects: Wind tunnels
Edition Identifiers:
- The Open Library ID: OL15385242M - OL14699970M - OL18064279M - OL17110561M
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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25A three-dimensional orthogonal laser velocimeter for the NASA Ames 7- by 10-foot wind tunnel
By Stephen E. Dunagan
“A three-dimensional orthogonal laser velocimeter for the NASA Ames 7- by 10-foot wind tunnel” Metadata:
- Title: ➤ A three-dimensional orthogonal laser velocimeter for the NASA Ames 7- by 10-foot wind tunnel
- Author: Stephen E. Dunagan
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va
“A three-dimensional orthogonal laser velocimeter for the NASA Ames 7- by 10-foot wind tunnel” Subjects and Themes:
- Subjects: ➤ Bragg cells - Fiber optics - Laser Doppler velocimeters - Optical fibers - Velocity measurement - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL17114772M - OL18079190M - OL16984304M - OL15409685M
- Online Computer Library Center (OCLC) ID: 32799687
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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26The 13-inch magnetic suspension and balance system wind tunnel
By William G. Johnson
“The 13-inch magnetic suspension and balance system wind tunnel” Metadata:
- Title: ➤ The 13-inch magnetic suspension and balance system wind tunnel
- Author: William G. Johnson
- Language: English
- Number of Pages: Median: 45
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Division - Langley Research Center
- Publish Date: 1989
- Publish Location: ➤ [Washington, DC] - Hampton, Va - [Springfield, Va
“The 13-inch magnetic suspension and balance system wind tunnel” Subjects and Themes:
- Subjects: Magnetic suspension - Subsonic wind tunnels - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL15284992M - OL17098599M - OL18031871M - OL18929472M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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27Wind-tunnel investigation of an advanced general aviation canard configuration
By Joseph R. Chambers
“Wind-tunnel investigation of an advanced general aviation canard configuration” Metadata:
- Title: ➤ Wind-tunnel investigation of an advanced general aviation canard configuration
- Author: Joseph R. Chambers
- Language: English
- Number of Pages: Median: 45
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1984
- Publish Location: ➤ [Springfield, Va - Washington, D.C
“Wind-tunnel investigation of an advanced general aviation canard configuration” Subjects and Themes:
- Subjects: Aerodynamics - Airplanes - Canard Wings - Wind tunnel models - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL18038976M - OL17079321M - OL15312575M - OL17127907M
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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28Wind-tunnel technique
By R. C. Pankhurst
“Wind-tunnel technique” Metadata:
- Title: Wind-tunnel technique
- Author: R. C. Pankhurst
- Language: English
- Number of Pages: Median: 702
- Publisher: Pitman
- Publish Date: 1952
- Publish Location: London
“Wind-tunnel technique” Subjects and Themes:
- Subjects: Wind tunnels
Edition Identifiers:
- The Open Library ID: OL19948776M - OL20877247M - OL17461585M - OL6116084M
- Online Computer Library Center (OCLC) ID: 2208166
- Library of Congress Control Number (LCCN): 52014571
Access and General Info:
- First Year Published: 1952
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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29Guide: Assessing Experimental Uncertainty
By American Institute of Aeronautics and As

“Guide: Assessing Experimental Uncertainty” Metadata:
- Title: ➤ Guide: Assessing Experimental Uncertainty
- Author: ➤ American Institute of Aeronautics and As
- Language: English
- Number of Pages: Median: 83
- Publisher: ➤ AIAA (American Institute of Aeronautics & Ast - AIAA (American Institute of Aeronautics & Astronautics)
- Publish Date: 2003 - 2004
“Guide: Assessing Experimental Uncertainty” Subjects and Themes:
- Subjects: ➤ Wind tunnels - Airplanes - Models - Testing - Standards - Uncertainty (Information theory) - Airplanes, models - Uncertainty (information theory)
Edition Identifiers:
- The Open Library ID: OL12135812M - OL12135811M
- Online Computer Library Center (OCLC) ID: 53369417
- Library of Congress Control Number (LCCN): 2003024006
- All ISBNs: 1563476630 - 1563476649 - 9781563476648 - 9781563476631
Access and General Info:
- First Year Published: 2003
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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30J-85 jet engine noise measured in the ONERA S1 wind tunnel and extrapolated to far field
By Paul T. Soderman
“J-85 jet engine noise measured in the ONERA S1 wind tunnel and extrapolated to far field” Metadata:
- Title: ➤ J-85 jet engine noise measured in the ONERA S1 wind tunnel and extrapolated to far field
- Author: Paul T. Soderman
- Language: English
- Number of Pages: Median: 179
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - Ames Research Center - For sale by the National Technical Information Service]
- Publish Date: 1991
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va - [Washington, DC]
“J-85 jet engine noise measured in the ONERA S1 wind tunnel and extrapolated to far field” Subjects and Themes:
- Subjects: Jet aircraft noise - Jet planes - Measurement - Noise - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL18034972M - OL15299423M - OL21335087M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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31Large-scale aeroacoustic research feasibility and conceptual design of test-section inserts for the Ames 80- by 120-foot wind tunnel
By Paul T. Soderman
“Large-scale aeroacoustic research feasibility and conceptual design of test-section inserts for the Ames 80- by 120-foot wind tunnel” Metadata:
- Title: ➤ Large-scale aeroacoustic research feasibility and conceptual design of test-section inserts for the Ames 80- by 120-foot wind tunnel
- Author: Paul T. Soderman
- Language: English
- Number of Pages: Median: 45
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - Ames Research Center - For sale by the National Technical Information Service]
- Publish Date: 1990
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va - [Washington, DC]
“Large-scale aeroacoustic research feasibility and conceptual design of test-section inserts for the Ames 80- by 120-foot wind tunnel” Subjects and Themes:
- Subjects: Aeroacoustics - Design and construction - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL18035044M - OL21334944M - OL15299714M
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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32A description of devices used in the study of wind erosion of soils
By A. P. Bocharov
“A description of devices used in the study of wind erosion of soils” Metadata:
- Title: ➤ A description of devices used in the study of wind erosion of soils
- Author: A. P. Bocharov
- Language: English
- Number of Pages: Median: 90
- Publisher: ➤ Oxonian Press - Oxonian - Balkema
- Publish Date: 1984
- Publish Location: Rotterdam - New Delhi
“A description of devices used in the study of wind erosion of soils” Subjects and Themes:
- Subjects: Meteorological instruments - Soil erosion - Wind erosion - Wind tunnels
- Places: Soviet Union
Edition Identifiers:
- The Open Library ID: OL3010585M - OL43737227M - OL15080978M
- Online Computer Library Center (OCLC) ID: 59726748
- Library of Congress Control Number (LCCN): 84905588
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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33Low-speed wind tunnel testing
By Jewel B. Barlow

“Low-speed wind tunnel testing” Metadata:
- Title: Low-speed wind tunnel testing
- Author: Jewel B. Barlow
- Language: English
- Number of Pages: Median: 713
- Publisher: ➤ Wiley - Wiley & Sons, Limited, John - WILEY
- Publish Date: 1999 - 2010
- Publish Location: New York
“Low-speed wind tunnel testing” Subjects and Themes:
- Subjects: Wind tunnels
Edition Identifiers:
- The Open Library ID: OL37109572M - OL368310M
- Library of Congress Control Number (LCCN): 98028891
- All ISBNs: 9780471557746 - 047050207X - 9780470502075 - 0471557749
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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34Wind-tunnel experiments on divergence of forward-swept wings
By Rodney H. Ricketts
“Wind-tunnel experiments on divergence of forward-swept wings” Metadata:
- Title: ➤ Wind-tunnel experiments on divergence of forward-swept wings
- Author: Rodney H. Ricketts
- Language: English
- Number of Pages: Median: 46
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1980
- Publish Location: ➤ [Springfield, Va. : For sale by the National Technical Information Service] - Washington, D.C
“Wind-tunnel experiments on divergence of forward-swept wings” Subjects and Themes:
- Subjects: Testing - Airplanes - Wings - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL17548109M - OL15258703M - OL18022863M
Access and General Info:
- First Year Published: 1980
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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35Force and moment flow-visualization, and boundary-layer tests on a Shuttle Orbiter model at Mach 6
By Robert L. Calloway
“Force and moment flow-visualization, and boundary-layer tests on a Shuttle Orbiter model at Mach 6” Metadata:
- Title: ➤ Force and moment flow-visualization, and boundary-layer tests on a Shuttle Orbiter model at Mach 6
- Author: Robert L. Calloway
- Language: English
- Number of Pages: Median: 23
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1981
- Publish Location: ➤ [Springfield, Va. : For sale by the National Technical Information Service] - Washington, D.C
“Force and moment flow-visualization, and boundary-layer tests on a Shuttle Orbiter model at Mach 6” Subjects and Themes:
- Subjects: Testing - Boundary layer - Wind tunnels - Reusable space vehicles
Edition Identifiers:
- The Open Library ID: OL15258729M - OL17548126M - OL18022880M
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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36The preliminary checkout, evaluation and calibration of a 3-component force measurement system for calibrating propulsion simulators for wind tunnel models
By William A. Scott
“The preliminary checkout, evaluation and calibration of a 3-component force measurement system for calibrating propulsion simulators for wind tunnel models” Metadata:
- Title: ➤ The preliminary checkout, evaluation and calibration of a 3-component force measurement system for calibrating propulsion simulators for wind tunnel models
- Author: William A. Scott
- Language: English
- Publisher: ➤ Flight Research Laboratory, University of Kansas, Center for Research Inc.
- Publish Date: 1984
- Publish Location: Lawrence, Kan
“The preliminary checkout, evaluation and calibration of a 3-component force measurement system for calibrating propulsion simulators for wind tunnel models” Subjects and Themes:
- Subjects: Ground simulators - Propulsion systems - Wind tunnels - Space vehicles
Edition Identifiers:
- The Open Library ID: OL17832119M - OL14929114M - OL17666831M
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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37Wind-tunnel free-flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps
By Long P. Yip
“Wind-tunnel free-flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps” Metadata:
- Title: ➤ Wind-tunnel free-flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps
- Author: Long P. Yip
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1987
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Wind-tunnel free-flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps” Subjects and Themes:
- Subjects: Testing - Wind tunnels - Stability of airplanes
Edition Identifiers:
- The Open Library ID: OL15275193M - OL16371450M - OL18029126M
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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38A wind-tunnel study of the applicability of far-field sonic-boom theory to the space shuttle orbiter
By Harry W. Carlson
“A wind-tunnel study of the applicability of far-field sonic-boom theory to the space shuttle orbiter” Metadata:
- Title: ➤ A wind-tunnel study of the applicability of far-field sonic-boom theory to the space shuttle orbiter
- Author: Harry W. Carlson
- Language: English
- Number of Pages: Median: 45
- Publisher: ➤ for sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1978
- Publish Location: [Washington] - Springfield, Va
“A wind-tunnel study of the applicability of far-field sonic-boom theory to the space shuttle orbiter” Subjects and Themes:
- Subjects: Wind tunnels - Sonic boom - Reusable space vehicles
Edition Identifiers:
- The Open Library ID: OL18013797M - OL15224983M - OL17537271M
Access and General Info:
- First Year Published: 1978
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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39Low-speed wind tunnel performance of high-speed counterrotation propellers at angle-of-attack
By Christopher E. Hughes
“Low-speed wind tunnel performance of high-speed counterrotation propellers at angle-of-attack” Metadata:
- Title: ➤ Low-speed wind tunnel performance of high-speed counterrotation propellers at angle-of-attack
- Author: Christopher E. Hughes
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration
- Publish Date: 1989
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Low-speed wind tunnel performance of high-speed counterrotation propellers at angle-of-attack” Subjects and Themes:
- Subjects: Aerial Propellers - Propellers, Aerial - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL17097260M - OL18030603M - OL15280028M
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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40In-situ technique for checking the calibration of platinum resistance thermometers
By Kamran Daryabeigi
“In-situ technique for checking the calibration of platinum resistance thermometers” Metadata:
- Title: ➤ In-situ technique for checking the calibration of platinum resistance thermometers
- Author: Kamran Daryabeigi
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1987
- Publish Location: Hampton, Va - [Springfield, Va
“In-situ technique for checking the calibration of platinum resistance thermometers” Subjects and Themes:
- Subjects: Wind tunnels - Resistance thermometers - Calibration
Edition Identifiers:
- The Open Library ID: OL17098950M - OL18032172M - OL15286192M
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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41User manual for 0.3-M TCT wall-interference assessment/correction procedure
By Clyde R. Gumbert
“User manual for 0.3-M TCT wall-interference assessment/correction procedure” Metadata:
- Title: ➤ User manual for 0.3-M TCT wall-interference assessment/correction procedure
- Author: Clyde R. Gumbert
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1985
- Publish Location: Hampton, Va - [Springfield, Va
“User manual for 0.3-M TCT wall-interference assessment/correction procedure” Subjects and Themes:
- Subjects: Wind tunnels
Edition Identifiers:
- The Open Library ID: OL17096482M - OL18029771M - OL15276764M
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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42Flight and wind-tunnel comparisons of the inlet/airframe interaction of the F-15 airplane
By Lannie D. Webb
“Flight and wind-tunnel comparisons of the inlet/airframe interaction of the F-15 airplane” Metadata:
- Title: ➤ Flight and wind-tunnel comparisons of the inlet/airframe interaction of the F-15 airplane
- Author: Lannie D. Webb
- Language: English
- Number of Pages: Median: 32
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
- Publish Date: 1984
- Publish Location: ➤ [Springfield, Va - Washington, D.C
“Flight and wind-tunnel comparisons of the inlet/airframe interaction of the F-15 airplane” Subjects and Themes:
- Subjects: Wind tunnels - Eagle (Jet fighter plane)
Edition Identifiers:
- The Open Library ID: OL17558805M - OL15321639M - OL18041453M
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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43Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section
By Robert J. McGhee
“Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section” Metadata:
- Title: ➤ Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section
- Author: Robert J. McGhee
- Language: English
- Number of Pages: Median: 84
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
- Publish Date: 1981
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section” Subjects and Themes:
- Subjects: Wind tunnels - Aerofoils
Edition Identifiers:
- The Open Library ID: OL17549330M - OL15261762M - OL18023750M
Author's Alternative Names:
"Robert J McGhee"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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44Wind-tunnel study of wind loading on a compliant offshore platform
By Thomas A. Morreale
“Wind-tunnel study of wind loading on a compliant offshore platform” Metadata:
- Title: ➤ Wind-tunnel study of wind loading on a compliant offshore platform
- Author: Thomas A. Morreale
- Language: English
- Number of Pages: Median: 28
- Publisher: ➤ The Standards - Order from National Technical Information Service (NTIS)
- Publish Date: 1984
- Publish Location: ➤ [Springfield, VA - Washington, DC
“Wind-tunnel study of wind loading on a compliant offshore platform” Subjects and Themes:
- Subjects: Aerodynamics - Wind tunnels - Offshore structures
Edition Identifiers:
- The Open Library ID: OL18037914M - OL17555487M - OL15309377M
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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45Wind-tunnel free-flight investigation of a supersonic persistence fighter
By David E. Hahne
“Wind-tunnel free-flight investigation of a supersonic persistence fighter” Metadata:
- Title: ➤ Wind-tunnel free-flight investigation of a supersonic persistence fighter
- Author: David E. Hahne
- Language: English
- Number of Pages: Median: 59
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - Langley Research Center
- Publish Date: 1993
- Publish Location: ➤ [Washington, DC] - [Springfield, Va - Hampton, Va
“Wind-tunnel free-flight investigation of a supersonic persistence fighter” Subjects and Themes:
- Subjects: Supersonic fighter planes - Fighter aircraft - Flight tests - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL18057551M - OL19247972M - OL15370906M
Access and General Info:
- First Year Published: 1993
- 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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46Experiments in a three-dimensional adaptive-wall wind tunnel
By Edward T. Schairer
“Experiments in a three-dimensional adaptive-wall wind tunnel” Metadata:
- Title: ➤ Experiments in a three-dimensional adaptive-wall wind tunnel
- Author: Edward T. Schairer
- Language: English
- Number of Pages: Median: 29
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
- Publish Date: 1983
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“Experiments in a three-dimensional adaptive-wall wind tunnel” Subjects and Themes:
- Subjects: Airplanes - Wind tunnels - Flight testing
Edition Identifiers:
- The Open Library ID: OL18036958M - OL17554193M - OL15306024M
Access and General Info:
- First Year Published: 1983
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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47Wind-tunnel investigation of aerodynamic efficiency of three planar ellipyical wings with curvature of quarter-chord line
By Raymond E. Mineck
“Wind-tunnel investigation of aerodynamic efficiency of three planar ellipyical wings with curvature of quarter-chord line” Metadata:
- Title: ➤ Wind-tunnel investigation of aerodynamic efficiency of three planar ellipyical wings with curvature of quarter-chord line
- Author: Raymond E. Mineck
- Language: English
- Publisher: ➤ National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1993
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Wind-tunnel investigation of aerodynamic efficiency of three planar ellipyical wings with curvature of quarter-chord line” Subjects and Themes:
- Subjects: Wind tunnels - Airplanes - Wings
Edition Identifiers:
- The Open Library ID: OL15384696M - OL18063974M - OL14699114M
Access and General Info:
- First Year Published: 1993
- 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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48Wind-tunnel investigation of a flush airdata system at Mach numbers from 0.7 to 1.4
By Terry J. Larson
“Wind-tunnel investigation of a flush airdata system at Mach numbers from 0.7 to 1.4” Metadata:
- Title: ➤ Wind-tunnel investigation of a flush airdata system at Mach numbers from 0.7 to 1.4
- Author: Terry J. Larson
- Language: English
- Number of Pages: Median: 31
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility
- Publish Date: 1990
- Publish Location: ➤ Edwards, Calif - Springfield, VA
“Wind-tunnel investigation of a flush airdata system at Mach numbers from 0.7 to 1.4” Subjects and Themes:
- Subjects: ➤ Aeronautical instruments - Algorithms - Flushing - Air data systems - Wind tunnel tests - Wind tunnels - Flight tests
Edition Identifiers:
- The Open Library ID: OL16138129M - OL18263198M - OL17630323M
- Online Computer Library Center (OCLC) ID: 25269779
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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49Dynamic wind-tunnel tests of an aeromechanical gust-alleviation system using several different combinations of control surfaces
By Eric C. Stewart
“Dynamic wind-tunnel tests of an aeromechanical gust-alleviation system using several different combinations of control surfaces” Metadata:
- Title: ➤ Dynamic wind-tunnel tests of an aeromechanical gust-alleviation system using several different combinations of control surfaces
- Author: Eric C. Stewart
- Language: English
- Number of Pages: Median: 34
- Publisher: ➤ for sale by the National Technical Information Office - National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1978
- Publish Location: Springfield, Va - [Washington]
“Dynamic wind-tunnel tests of an aeromechanical gust-alleviation system using several different combinations of control surfaces” Subjects and Themes:
- Subjects: Gust loads - Dynamics - Wind tunnels - Airplanes
Edition Identifiers:
- The Open Library ID: OL17797543M - OL17647811M - OL18013884M
Access and General Info:
- First Year Published: 1978
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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50Summary of low-speed wind tunnel results of several high-speed counterrotation propeller configurations
By Christopher G. Hughes
“Summary of low-speed wind tunnel results of several high-speed counterrotation propeller configurations” Metadata:
- Title: ➤ Summary of low-speed wind tunnel results of several high-speed counterrotation propeller configurations
- Author: Christopher G. Hughes
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration
- Publish Date: 1988
- Publish Location: [Washington, DC]
“Summary of low-speed wind tunnel results of several high-speed counterrotation propeller configurations” Subjects and Themes:
- Subjects: Aerial Propellers - Propellers, Aerial - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL14664525M - OL18029458M - OL15275865M
Access and General Info:
- First Year Published: 1988
- 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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Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Wind tunnel
inventor Poul la Cour used wind tunnels to develop wind turbines in the early 1890s. Carl Rickard Nyberg used a wind tunnel to design his Flugan starting
Vertical wind tunnel
A vertical wind tunnel (VWT) is a wind tunnel that moves air up in a vertical column. Unlike standard wind tunnels, which have test sections that are
List of wind tunnels
This is an alphabetical list of wind tunnels. "A2 wind tunnel". Retrieved 26 January 2024. "ACE Climatic Wind Tunnel". Retrieved 26 January 2024. "Fly
Hypersonic wind tunnel
facilities like blow-down wind tunnels are designed and installed to simulate the hypersonic flow. A hypersonic wind tunnel comprises in flow direction
Supersonic wind tunnel
supersonic wind tunnel is enormous, of the order of 50 MW per square meter of test section cross-sectional area. For this reason, most wind tunnels operate
Propulsion Wind Tunnel Facility
Propulsion Wind Tunnel Facility, located at Arnold Engineering Development Complex, Arnold Air Force Base, Tennessee, holds three wind tunnels: the 16-foot
Compressible flow
principle behind the wind tunnel is that a large pressure difference is maintained upstream to downstream, driving the flow. Wind tunnels can be divided into
European Transonic Wind Tunnel
transonic wind tunnel (ETW) is a high-Reynolds-number transonic wind tunnel using nitrogen as the test gas. It is one of the world's largest cryogenic wind tunnels
Trisonic Wind Tunnel
known trisonic wind tunnel was dated to 1950 and was located in El Segundo, California before it closed in 2007. Other trisonic wind tunnels currently in
German Aeronautical Research Institute
Institute of Aerodynamics had five wind tunnels, while the Institute of Gas Dynamics had its own high-speed tunnel; both were at the southern end of the