The design, fabrication, and adaptation of a model damper system to the 5.5% aeroelastic model of the Saturn 1B/Skylab launch vehicle are reported. The damper is dynamically calibrated over the desired range of additive damping for model conditions prior to wind tunnel testing. (Author)
Electromagnetic Damper System for Ground Wind Load Studies
1972
61 pages
Report
No indication
English
Space Shuttle Damper System for Ground Wind Load Tests
NTIS | 1973
|Space Shuttle Damper System for Ground Wind Load Tests
NTRS | 1973
|