Forced response prediction for industrial gas turbine blades [PDF]
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]
Afzal A +5 more
europepmc +1 more source
Axial and Centrifugal Compressor Mean Line Flow Analysis Method
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]
Zhang Z +6 more
europepmc +1 more source
Experimental Study to Quantify Fracture Propagation in Hydraulic Fracturing Treatment. [PDF]
He P, Pan L, Lu Z, Zhou J, Meng C, Yu H.
europepmc +1 more source
A Resistivity Plate Loading Device for Assessing the Factors Affecting the Stiffness of a Cement-Stabilized Subgrade. [PDF]
Feng H, Siaw AF, Wang H.
europepmc +1 more source
Performance of NACA Eight-stage Axial-flow Compressor Designed on the Basis of Airfoil Theory
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
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
Natalie R. Smith, Nicole L. Key
openaire +1 more source
Study on the stability enhancement mechanism of a high-speed axial compressor under paired swirl distortion. [PDF]
Cheng B, Li Y, Yin Z, Yu Y, Liu J.
europepmc +1 more source

