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There are a total of 38 record(s) matching your query.
Sorted by: Date Added To NTRS in Descending order
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Aerodynamics of a linear oscillating cascade
Author(s): Buffum, Daniel H.; Fleeter, Sanford
Abstract: The steady and unsteady aerodynamics of a linear oscillating cascade are investigated using experimental and computational methods. Experiments are performed to quantify the torsion mode oscillating cascade aerodynamics of ...
NASA Center: Glenn Research Center Publication Year: 1990
Added to NTRS: 2005-10-13
Accession Number: 90N27657; Document ID: 19900018341; Report Number: E-5677, NAS 1.15:103250, NASA-TM-103250
Active Suppression of Aerodynamic Instabilities in Centrifugal Compressors
Author(s): Fleeter, Sanford
Abstract: The operating range of a compressor is bounded by the surge and choke lines on a performance map. The barrier posed by the surge line is of particular interest due to its proximity to the maximum efficiency points of the ...
NASA Center: Glenn Research Center Publication Year: 1994
Added to NTRS: 2005-08-25
Accession Number: 97N72520; Document ID: 19970040808; Report Number: NAS 1.26:206024, NASA/CR-97-206024
Wind tunnel wall effects in a linear oscillating cascade
Author(s): Buffum, Daniel H.; Fleeter, Sanford
Abstract: Experiments in a linear oscillating cascade reveal that the wind tunnel walls enclosing the airfoils have, in some cases, a detrimental effect on the oscillating cascade aerodynamics. In a subsonic flow field, biconvex ...
NASA Center: Glenn Research Center Publication Year: 1991
Added to NTRS: 2005-08-25
Accession Number: 91N19098; Document ID: 19910009785; Report Number: E-5909, NAS 1.15:103690, NASA-TM-103690
Effect of wind tunnel acoustic modes on linear oscillating cascade aerodynamics
Author(s): Buffum, Daniel H.; Fleeter, Sanford
Abstract: The aerodynamics of a biconvex airfoil cascade oscillating in torsion is investigated using the unsteady aerodynamic influence coefficient technique. For subsonic flow and reduced frequencies as large as 0.9, airfoil surface ...
NASA Center: Glenn Research Center Publication Year: 1993
Added to NTRS: 2005-08-25
Accession Number: 94N15866; Document ID: 19940011393; Report Number: E-8171, NAS 1.15:106367, NASA-TM-106367
Experimental investigation of transonic oscillating cascade aerodynamics
Author(s): Buffum, Daniel H.; Fleeter, Sanford
Abstract: Fundamental experiments are performed in the NASA Lewis Transonic Oscillating Cascade Facility to investigate the subsonic and transonic aerodynamics of cascaded airfoils executing torsion mode oscillations at realistic ...
NASA Center: Glenn Research Center Publication Year: 1989
Added to NTRS: 2005-08-25
Accession Number: 89N20133; Document ID: 19890010762; Report Number: E-4697, NAS 1.15:101993, NASA-TM-101993
The effect of prewhirl on the internal aerodynamics and performance of a mixed flow research centrifugal compressor
Author(s): Bryan, William B.; Fleeter, Sanford
Abstract: The internal three-dimensional steady and time-varying flow through the diffusing elements of a centrifugal impeller were investigated using a moderate scale, subsonic, mixed flow research compressor facility. The ...
NASA Center: NASA (non Center Specific) Publication Year: 1987
Added to NTRS: 2005-08-25
Accession Number: 89N19503; Document ID: 19890010132; Report Number: AVSCOM-TR-87-C-35, ME-TSPC-TR-87-13, NAS 1.26:184756, NASA-CR-184756
Unsteady aerodynamics of an oscillating cascade in a compressible flow field
Author(s): Buffum, Daniel H.; Boldman, Donald R.; Fleeter, Sanford
Abstract: Fundamental experiments were performed in the NASA Lewis Transonic Oscillating Cascade Facility to investigate and quantify the unsteady aerodynamics of a cascade of biconvex airfoils executing torsion-mode oscillations at ...
NASA Center: Glenn Research Center Publication Year: 1987
Added to NTRS: 2005-08-25
Accession Number: 88N13346; Document ID: 19880003964; Report Number: E-3830, NAS 1.15:100219, NASA-TM-100219
Unsteady incompressible aerodynamics and forced response of detuned blade rows
Author(s): Chiang, Hsiao-Wei D.; Fleeter, Sanford
Abstract: A mathematical model is developed and utilized to demonstrate the enhanced forced response behavior associated with aerodynamic, structural, and combined aerodynamic-structural detuning of a loaded rotor operating in an ...
NASA Center: NASA (non Center Specific) Publication Year: 1990
Added to NTRS: 2004-11-03
Accession Number: 90A19805; Document ID: 19900032750; Report Number: AIAA PAPER 90-0340
Simultaneous Active Source Control of Blade Row Interaction Generated Discrete Tones
Author(s): Sawyer, Scott; Fleeter, Sanford
Abstract: Unsteady blade row interactions in turbomachines generate discrete-frequency tones at blade pass frequency and its harmonics. Specific circumferential acoustic modes are generated. However, only certain of these modes ...
NASA Center: Glenn Research Center Publication Year: 1999
Added to NTRS: 2004-11-03
Document ID: 20000020802
Forcing function modeling for flow induced vibration
Author(s): Fleeter, Sanford
Abstract: The fundamental forcing function unsteady aerodynamics for application to turbomachine blade row forced response are considered, accomplished through a series of experiments performed in a rotating annular cascade and a ...
NASA Center: Glenn Research Center Publication Year: 1993
Added to NTRS: 2004-11-03
Accession Number: 93A54003; Document ID: 19930070006; Report Number: ISABE 93-7027
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