An improved blade passage model for estimating off-design axial compressor performance

Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2013.

Bibliographic Details
Main Author:	Brand, Maximilian Lewis
Other Authors:	Zoltán S. Spakovszky.
Format:	Thesis
Language:	eng
Published:	Massachusetts Institute of Technology 2014
Subjects:	Aeronautics and Astronautics.
Online Access:	http://hdl.handle.net/1721.1/85765

Similar Items

Blade passage flow structure effects on axial compressor rotating stall inception
by: Hoying, Donald Andrew
Published: (2005)

Non-uniform radial meanline method for off-design performance estimation of multistage axial compressors
by: Birkenheier, David Andrew
Published: (2018)

Improved return passages for multistage centrifugal compressors
by: Glass, Benjamin W., S.M. Massachusetts Institute of Technology
Published: (2011)

Design of an active compressor blade for aeroelastic studies
by: Maahs, Gordon Lewis, 1974-
Published: (2009)

Effect of a sinusoidal three-lobe total pressure distortion on a transonic compressor : distortion propagation, compressor performance, and blade passage events
by: MacLeod, Brenda Brennan, 1971-
Published: (2013)

Robust design and tolerancing of compressor blades
by: Dow, Eric Alexander
Published: (2015)

Axial compressor reversed flow performance
by: Gamache, Robert Normand
Published: (2005)

A computational model for multistage axial compressor design
by: Wisnia, Arnaud Irving
Published: (2010)

Time resolved measurements of rotating stall in axial flow compressors
by: Lavrich, Philip Lewis
Published: (2005)

Design and analysis of axial aspirated compressor stages
by: Merchant, Ali A. (Ali Abbas)
Published: (2005)

Probabilistic performance-based geometric tolerancing of compressor blades
by: Lamb, Caroline Marie
Published: (2006)

Implications of stability modeling for high-speed axial compressor design
by: Fréchette, Luc G. (Luc Guy)
Published: (2005)

Endwall blockage in axial compressors
by: Khalsa, Amrit Singh
Published: (2005)

Blade passage flow structure effects on axial compressor rotating stall inception
by: Hoying, Donald Andrew
Published: (2016)

Applications of axial and radial compressor dynamic system modeling
by: Spakovszky, Zoltán S. (Zoltán Sándor), 1972-
Published: (2005)

Blade row interaction effects on compressor measurements
by: Shang, Tonghuo
Published: (2008)

Estimation of axial compressor body forces using three-dimensional flow computations
by: Reichstein, Georg A
Published: (2009)

Application of an energy-like stability metric for axial compressor design
by: Dorca Luque, Josep M. (Josep Maria), 1981-
Published: (2013)

Investigation of mixing in a multistage axial compressor
by: Digavalli, Sasi K. (Sasi Kumar)
Published: (2008)

Active control of rotating stall in axial compressors
by: Paduano, James D. (James Donald)
Published: (2005)

Manufacturing and testing of an active compressor blade for aeroelastic studies
by: Sahoo, Debashis, 1976-
Published: (2005)

Evaluation of rotating stall warning schemes for axial compressors
by: Etchevers, Olivier
Published: (2005)

Role of tip clearance flow on axial compressor stability
by: Vo, Huu Duc, 1971-
Published: (2005)

Active control of tip clearance flow in axial compressors
by: Bae, Jinwoo W
Published: (2005)

Dynamic stability analysis of a multi-stage axial compressor with design implications
by: Blanvillain, Emmanuel, 1979-
Published: (2013)

Modeling and control of rotating stall in high speed multi-stage axial compressors
by: Feulner, Matthew Roger, 1967-
Published: (2005)

The effect of upstream rotor vortical disturbances on the time-average performance of axial compressor stators
by: Valkov, Theodore V. (Theodore Valkov)
Published: (2009)

Small core axial compressors for high efficiency jet aircraft
by: DiOrio, Austin Graf
Published: (2013)

Actuation for rotating stall control of high speed axial compressors
by: Berndt, Roland Günter
Published: (2005)

Robust control of a surge and rotating stall in an axial compressor
by: Liao, Shengfang, 1968-
Published: (2005)

Fabrication and testing of a spar-actuated active compressor rotor blade
by: Lin, Yiben
Published: (2013)

CFD investigation of transonic axial compressor rotor blade at various off-design conditions
by: Epsipha, Pauline, et al.
Published: (2016)

Tip clearance effects on multistage axial compressor performance and flow structure for small core application
by: Koff, Andrew (Andrew Steven)
Published: (2017)

A simple criterion for three-dimensional flow separation in axial compressors
by: Lei, Vai-Man
Published: (2007)

Characterization of wake- and tip-vortex-induced unsteady blade response in multistage compressor environment
by: Lenglin, Geoffroy (Geoffroy Philippe), 1976-
Published: (2013)

An experimental study of blade tip clearance suction applied to a high speed compressor
by: Dennis, Joseph E. (Joseph Eric)
Published: (2009)

Dynamic control of rotating stall in axial flow compressors using aeromechanical feedback
by: Gysling, Daniel Lawrence
Published: (2005)

Effect of circumferential groove casing treatment parameters on axial compressor flow range
by: Hanley, Brian K. (Brian Kyle)
Published: (2010)

Vibration and crack detection in gas turbine engine compressor blades using Eddy current sensors
by: Lackner, Matthew, 1980-
Published: (2005)

Active control of rotating stall in a three-stage axial compressor with jet actuators
by: Vo, Huu Duc, 1971-
Published: (2009)