Search results for: Bangert, Linda S.
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1
Effects of afterbody boattail design and empennage arrangement on aeropropulsive characteristics of a twin-engine fighter model at transonic speeds
Authors: Bangert, Linda S.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1987Physical Description: 1 volume.Holdings: Loading…
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2
Effect of afterbody geometry on aerodynamic characteristics of isolated nonaxisymmetric afterbodies at transonic Mach numbers
Authors: Bangert, Linda S.
Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [For sale by the National Technical Information Service], 1992Physical Description: 1 volume.Holdings: Loading…
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3
Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability
Authors: Bangert, Linda S.
Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989Physical Description: 1 volume., Also available via Internet from the NTRS web site. Address as of 4/28/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890018263%5F1989018263.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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4
Static investigation of circular-to-rectangular transition ducts for high-aspect-ratio nonaxisymmetric nozzles
Authors: Burley, James R.Other Authors: “…Bangert, Linda S.…”
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service, 1986
Physical Description: 1 volume.Holdings: Loading…
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5
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.Other Authors:
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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Related Subjects
Wind tunnel tests
Fighter planes
Static tests
Testing
Aerodynamic measurements
Air ducts
Calibrating
Chokes (fuel systems)
Deflectors
Drag (Aerodynamics)
Equipment and supplies
Flow deflection
High aspect ratio
Jet nozzles
Jet planes
Nozzle design
Nozzle flow
Nozzles
Thrust reversal
Thrust reversers
Thrust vector control
Transonic wind tunnels
Venturi tubes
Weight (Mass)