Search results for: Hill, Acquilla S.
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1
Calibration of the 13- by 13-inch adaptive wall test section for the Langley 0.3-Meter Transonic Cryogenic Tunnel
Authors: Mineck, Raymond E.Other Authors: “…Hill, Acquilla S.…”
Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1990
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2
High Reynolds number transonic tests of an NACA 0012 airfoil in the Langley 0.3-meter transonic cryogenic tunnel
Authors: Ladson, Charles L.Other Authors: “…Hill, Acquilla S.…”
Published: National Aeronautics and Space Administration, Langley Research Center, 1987
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3
Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
Authors: Johnson, William G. (William Garland), 1944-Other Authors: “…Hill, Acquilla S.…”
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1985
Physical Description: 1 volume., Also available via Internet from the NTRS web site. Address as of 9/04/07: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19860006729%5F1986006729.pdf ; current access is available via PURL.Holdings: Loading…Connect to: PDF version - All users (Federal Depository Library Program Persistant URL)
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4
Pressure distributions from high Reynolds number tests of a NASA SC(3)-0712(B) airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
Authors: Johnson, William G. (William Garland), 1944-Other Authors: “…Hill, Acquilla S.…”
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1985
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5
High Reynolds number tests of a NASA SC(3)-0712(b) airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnels
Authors: Johnson, William G. (William Garland), 1944-Other Authors: “…Hill, Acquilla S.…”
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1985
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6
CAST-10-2/DOA 2 Airfoil Studies Workshop results : proceedings of a workshop sponsored by the National Aeronautics and Space Administration and held at NASA Langley Research Center...
Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [National Technical Information Service, distributor], 1989Other Authors:Physical Description: 1 volume.Holdings: Loading…
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7
Tests of a NACA 65₁-213 airfoil in the NASA Langley 0.3 meter transonic cryogenic tunnel
Authors: Plentovich, Elizabeth B.Other Authors:
Published: National Aeronautics and Space Administration, Langley Research Center, 1984Physical Description: 1 volume.Holdings: Loading…
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8
Pressure distributions from high Reynolds number transonic tests of an NACA 0012 airfoil in the Langley 0.3-meter transonic cryogenic tunnel
Authors: Ladson, Charles L.Other Authors: “…Hill, Acquilla S.…”
Published: National Aeronautics and Space Administration, Langley Research Center, 1987
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Related Subjects
Aerofoils
Aerodynamics, Transonic
Reynolds number
Transonic wind tunnels
Testing
Aerodynamic characteristics
Aerodynamics
Airfoil profiles
Airfoils
Boeing aircraft
Calibration
Cryogenic wind tunnels
High Reynolds number
Pressure distribution
Supercritical airfoils
Two dimensional bodies
Wind tunnel models
Wind tunnel tests
Wind tunnel walls