Add to ORKGAn analysis of dynamic test data from vibration testing of a number of aerospace vehicles was made to develop an empirical structural damping law. A systematic attempt was made to fit dissipated energy/cycle to combinations of all dynamic variables. The best-fit laws for bending, torsion, and longitudinal motion are given, with error bounds. A discussion and estimate are made of error sources. Programs are developed for predicting equivalent linear structural damping coefficients and finding the response of nonlinearly damped structures
A spacecraft payload flown on a launch vehicle experiences dynamic loads. The dynamic loads are caus...
Damping in multiple beam structural vibration analysis - steady state analysis and transient vibrati...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.In...
A dissipative energy approach for predicting the damping of four-component space shuttle model by me...
Analytical and experimental study of dynamic responses of structures with nonlinear and nonproportio...
An empirical method is developed for predicting the modal damping of a combined parallel-stage shutt...
The space shuttle introduced a new dimension in the complexity of the structural dynamics of a space...
Accelerometer data were collected during on-orbit structural dynamic testing of the Solar Array Flig...
This report examines some aspects of the lack of close correlation between the predictions of analyt...
This report examines some aspects of the lack of close correlation between the predictions of analyt...
Vibration tests and analyses of six 1/8 scale models of the space shuttle solid rocket boosters are ...
The effect of localized structural damping on the excitability of higher order normal modes of the l...
Displacement, velocity, and acceleration admittances were calculated for a realistic NASTRAN structu...
The proceedings of the 58th Shock and Vibration Symposium, held in Huntsville, Alabama, October 13 ...
The work reported here is directed towards the problem of measuring and modeling non-linear damping...
A spacecraft payload flown on a launch vehicle experiences dynamic loads. The dynamic loads are caus...
Damping in multiple beam structural vibration analysis - steady state analysis and transient vibrati...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.In...
A dissipative energy approach for predicting the damping of four-component space shuttle model by me...
Analytical and experimental study of dynamic responses of structures with nonlinear and nonproportio...
An empirical method is developed for predicting the modal damping of a combined parallel-stage shutt...
The space shuttle introduced a new dimension in the complexity of the structural dynamics of a space...
Accelerometer data were collected during on-orbit structural dynamic testing of the Solar Array Flig...
This report examines some aspects of the lack of close correlation between the predictions of analyt...
This report examines some aspects of the lack of close correlation between the predictions of analyt...
Vibration tests and analyses of six 1/8 scale models of the space shuttle solid rocket boosters are ...
The effect of localized structural damping on the excitability of higher order normal modes of the l...
Displacement, velocity, and acceleration admittances were calculated for a realistic NASTRAN structu...
The proceedings of the 58th Shock and Vibration Symposium, held in Huntsville, Alabama, October 13 ...
The work reported here is directed towards the problem of measuring and modeling non-linear damping...
A spacecraft payload flown on a launch vehicle experiences dynamic loads. The dynamic loads are caus...
Damping in multiple beam structural vibration analysis - steady state analysis and transient vibrati...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.In...