Add to ORKGTechnical description of the effects of the fan assembly, excitation techniques, and procedures for reading the results, when the determination of resonant frequencies and forms of the corresponding mode, for fans rigidly attached to a base of inertia. Discussion of results for fans 3, 4, 5 and 6 blade
The objective of this thesis is to develop test and analysis procedures to revise ASHRAE Standard 87...
The paper discusses geometrical characteristics and strength parameters of fan blades equipped with ...
A three-dimensional linear frequency domain panel method has been extended to study the unsteady aer...
Technical description of the effects of the fan assembly, excitation techniques, and procedures for ...
Description of the technical effects of the fan assembly, excitation techniques, and procedures for ...
Test procedures and a mounting configuration for the vibration testing of propeller fans have been d...
Vibration modes associated with a fan impeller, motor, and motor mounting assembly in small air-cond...
The Finite Element Method is used to determine the fundamental mode shapes and frequencies of fan st...
A general analysis of the added mass and damping of a marine propeller in all modes of rigid body vi...
Aircraft engine blades are subject to harmonic forcing produced from periodic wakes created by fixed...
Nonoperating and operating vibration test procedures have been developed that can be used to identif...
Analytical models have been developed that can be used to investigate the vibration modes that exist...
Forced response is the main reason for high cycle fatigue in turbomachinery. Not all resonance point...
The exact mathematical treatment of the problem is possible by replacing the propeller blade by a ho...
A method has been devised for determining the frequencies of the various modes of a stationary prope...
The objective of this thesis is to develop test and analysis procedures to revise ASHRAE Standard 87...
The paper discusses geometrical characteristics and strength parameters of fan blades equipped with ...
A three-dimensional linear frequency domain panel method has been extended to study the unsteady aer...
Technical description of the effects of the fan assembly, excitation techniques, and procedures for ...
Description of the technical effects of the fan assembly, excitation techniques, and procedures for ...
Test procedures and a mounting configuration for the vibration testing of propeller fans have been d...
Vibration modes associated with a fan impeller, motor, and motor mounting assembly in small air-cond...
The Finite Element Method is used to determine the fundamental mode shapes and frequencies of fan st...
A general analysis of the added mass and damping of a marine propeller in all modes of rigid body vi...
Aircraft engine blades are subject to harmonic forcing produced from periodic wakes created by fixed...
Nonoperating and operating vibration test procedures have been developed that can be used to identif...
Analytical models have been developed that can be used to investigate the vibration modes that exist...
Forced response is the main reason for high cycle fatigue in turbomachinery. Not all resonance point...
The exact mathematical treatment of the problem is possible by replacing the propeller blade by a ho...
A method has been devised for determining the frequencies of the various modes of a stationary prope...
The objective of this thesis is to develop test and analysis procedures to revise ASHRAE Standard 87...
The paper discusses geometrical characteristics and strength parameters of fan blades equipped with ...
A three-dimensional linear frequency domain panel method has been extended to study the unsteady aer...