Contrails
The goal of the Contrails project is to help preserve and disseminate the technical record of 20th century aerospace research, highlighting in particular the research endeavors of the Illinois Tech community.

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6 reports

Experimental Modal Analysis and Dynamic Component Synthesis. Volume 1. Summary of Technical Work

Author(s): Randall J. Allenmang; David L. Brown
Corporate Author: University of Cincinnati
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1987-12
Report Number: AFWAL TR 87-3069 Volume 1
full text unavailable

Experimental Modal Analysis and Dynamic Component Synthesis. Volume 2. Measurement Techniques for Experimental Modal Analysis

Author(s): Randall J. Allenmang; David L. Brown; Robert W. Rost
Corporate Author: University of Cincinnati
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1987-12
Report Number: AFWAL TR 87-3069 Volume 2
full text unavailable

Experimental Modal Analysis and Dynamic Component Synthesis. Volume 3. Modal Parameter Estimation

Author(s): Randall J. Allenmang; David L. Brown
Corporate Author: University of Cincinnati
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1987-12
Report Number: AFWAL TR 87-3069 Volume 3
full text unavailable

Experimental Modal Analysis and Dynamic Component Synthesis. Volume 4. System Modeling Techniques

Author(s): Randall J. Allenmang; David L. Brown
Corporate Author: University of Cincinnati
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1987-12
Report Number: AFWAL TR 87-3069 Volume 4
full text unavailable

Experimental Modal Analysis and Dynamic Component Synthesis. Volume 5. Universal File Formats

Author(s): Randall J. Allenmang; David L. Brown
Corporate Author: University of Cincinnati
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1987-12
Report Number: AFWAL TR 87-3069 Volume 5
full text unavailable

Experimental Modal Analysis and Dynamic Component Synthesis. Volume 6. Software User's Guide

Author(s): Randall J. Allenmang; David L. Brown
Corporate Author: University of Cincinnati
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1987-12
Report Number: AFWAL TR 87-3069 Volume 6
full text unavailable