Search results for: Berrier, Bobby L.
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1
Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft
Authors: Berrier, Bobby L.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; 1980Physical Description: 215 pages : chiefly illustrations ; 27 cm.Holdings: Loading…
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2
Effect of several geometric parameters on the static internal performance of three nonaxisymmetric nozzle concepts
Authors: Berrier, Bobby L.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1979Physical Description: 134 pages : illustrations ; 27 cm.Holdings: Loading…
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3
Effect of port corner geometry on the internal performance of a rotating-vane-type thrust reverser
Authors: Berrier, Bobby L.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1986Physical Description: 1 volume.Holdings: Loading…
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4
Static internal performance of single-expansion-ramp nozzles with thrust-vectoring capability up to 60.
Authors: Berrier, Bobby L.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1984Physical Description: 1 volume.Holdings: Loading…
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5
Static performance of an axisymmetric nozzle with post-exit vanes for multiaxis thrust vectoring
Authors: Berrier, Bobby L.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1988Physical Description: 1 volume.Holdings: Loading…
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6
Internal performance of two nozzles utilizing gimbal concepts for thrust vectoring
Authors: Berrier, Bobby L.
Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1990Physical Description: 1 volume.Holdings: Loading…
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7
Operating characteristics of the multiple critical venturi system and secondary calibration nozzles used for weight-flow measurements in the Langley 16-foot transonic tunnel
Authors: Berrier, Bobby L.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985Physical Description: 1 volume., Also available via Internet from the NTRS web site. Address as of 07/07/08: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19860000549%5F1986000549.pdf ; current access is available via PURL.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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8
High Reynolds number investigation of a flush-mounted, S-duct inlet with large amounts of boundary layer ingestion
Authors: Berrier, Bobby L.
Published: National Aeronautics and Space Administration, Langley Research Center, 2005Physical Description: 1 online resource (165 pages) : illustrations (some color).Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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9
Effect of plug and shroud geometry variables on plug-nozzle performance at transonic speeds
Authors: Berrier, Bobby L.
Published: National Aeronautics and Space Administration, 1969Physical Description: 1 online resource (195 pages) : illustrations.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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10
Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft
Authors: Berrier, Bobby L., Re, Richard J.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980Physical Description: 1 online resource (215 pages) : chiefly illustrations.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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11
Static internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60°
Authors: Berrier, Bobby L., Leavitt, Laurence D.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1984Physical Description: 1 online resource (141 pages) : illustrations.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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12
Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles
Authors: Mason, Mary L., Berrier, Bobby L.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985Physical Description: 1 online resource (216 pages) : illustrations.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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13
Transonic aerodynamic characteristics of powered models of several Apollo launch-escape vehicle configurations
Authors: Berrier, Bobby L., Pendergraft, Odis C.
Published: National Aeronautics and Space Administration, Langley Research Center, 1968Physical Description: 1 online resource (41 pages, 1 unnumbered page) : illustrations.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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14
Static internal performance of single expansion-ramp nozzles with thrust vectoring and reversing
Authors: Re, Richard J.Other Authors: “…Berrier, Bobby L.…”
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982
Physical Description: 140 pages : illustrations ; 28 cm.Holdings: Loading…
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15
Investigation of axisymmetric and nonaxisymmetric nozzels installed on a 0.10-scale F-18 protype airplane model
Authors: Capone, Francis J.Other Authors: “…Berrier, Bobby L.…”
Published: National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1980
Physical Description: 301 pages : illustrations ; 28 cm.Holdings: Loading…
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16
Static performance of nonaxisymmetric nozzles with yaw thrust-vectoring vanes
Authors: Mason, Mary L.Other Authors: “…Berrier, Bobby L.…”
Published: National Aeronautics and Space Administration, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1988
Physical Description: 1 volume.Holdings: Loading…
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17
Effects of tail span and empennage arrangement on drag of a typical single-engine fighter aft end
Authors: Burley, James R.Other Authors: “…Berrier, Bobby L.…”
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1984
Physical Description: 1 volume.Holdings: Loading…
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18
Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane
Authors: Reubush, David E.Other Authors: “…Berrier, Bobby L.…”
Published: National Aeronautics and Space Administration, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1987
Physical Description: 1 volume.Holdings: Loading…
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19
Investigation of installation effects on single-engine convergent-divergent nozzles
Authors: Burley, James R.Other Authors: “…Berrier, Bobby L.…”
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982
Physical Description: 231 pages : illustrations ; 28 cm.Holdings: Loading…
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20
Investigation of installation effects on twin-engine convergent-divergent nozzles
Authors: Bare, E. AnnOther Authors: “…Berrier, Bobby L.…”
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1983
Physical Description: 188 pages : illustrations ; 28 cm.Holdings: Loading…
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Related Subjects
Aerodynamics
Jet nozzles
Testing
Airplanes
Convergent-divergent nozzles
Motors
Nozzles
Static tests
Thrust
Thrust vector control
Transonic wind tunnels
Wind tunnel tests
Yawing (Aerodynamics)
Fighter planes
Jet planes
Mach number
Nozzle design
Space vehicles
Thrust reversers
Yaw
Aerodynamic characteristics
Aerodynamic configurations
Aerodynamic measurements
Aerodynamics, Supersonic
Aerodynamics, Transonic
Aerospace vehicles
Air flow
Axisymmetric bodies
Blades
Boundary layers