NASA NTRS · 19710000210
Rotordynamic response analysis program
Abstract
Computer routine is similar to Holzer's method in torsional vibration treatment, and Prohl's and Myklestad's approach in computing rotor deflection. Matrix iteration technique is used to compute rotordynamic response by a simulated discrete mass system.
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Shen, F. A.. 1971-07-01. Rotordynamic response analysis program. https://ntrs.nasa.gov/citations/19710000210
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