Results 121 to 130 of about 631 (221)

Forced response prediction for industrial gas turbine blades [PDF]

open access: yes, 2006
A highly efficient aeromechanical forced response system is developed for predicting resonant forced vibration of turbomachinery blades with the capabilities of fully 3-D non-linear unsteady aerodynamics, 3-D finite element modal analysis and blade root ...
Moffatt, Stuart
core  

A critical review on renewable battery thermal management system using heat pipes. [PDF]

open access: yesJ Therm Anal Calorim, 2023
Afzal A   +5 more
europepmc   +1 more source

Axial and Centrifugal Compressor Mean Line Flow Analysis Method

open access: yes, 2009
This paper describes a method to estimate key aerodynamic parameters of single and multistage axial and centrifugal compressors. This mean-line compressor code COMDES provides the capability of sizing single and multistage compressors quickly during the ...
Veres, Joseph P.
core   +1 more source

Pneumatically Actuated Soft Gripper with Bistable Structures. [PDF]

open access: yesSoft Robot, 2022
Zhang Z   +6 more
europepmc   +1 more source

Performance of NACA Eight-stage Axial-flow Compressor Designed on the Basis of Airfoil Theory

open access: yes, 1943
The NACA has conducted an investigation to determine the performance that can be obtained from a multistage axial-flow compressor based on airfoil research.
Schey, Oscar W   +2 more
core   +1 more source

Unsteady Flow Field in a Multistage Axial Flow Compressor

open access: yes, 1997
The flow field in a multistage compressor is three-dimensional, unsteady, and turbulent with substantial viscous effects. Some of the specific phenomena that has eluded designers include the effects of rotor-stator and rotor-rotor interactions and the ...
Prato, J.   +2 more
core   +1 more source

Poster: Boundary Layer Separations in a Multistage Axial Compressor

open access: yes67th Annual Meeting of the APS Division of Fluid Dynamics - Gallery of Fluid Motion, 2014
Natalie R. Smith, Nicole L. Key
openaire   +1 more source

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