Search NASAโŒ• Search

NASA NTRS ยท 19800006869

Direct integration of transient rotor dynamics

Abstract

An implicit method was developed for integrating the equations of motion for a lumped mass model of a rotor dynamics system. As an aside, a closed form solution to the short bearing theory was also developed for a damper with arbitrary motion. The major conclusions are that the method is numerically stable and that the computation time is proportional to the number of elements in the rotor dynamics model rather than to the cube of the number. This computer code allowed the simulation of a complex rotor bearing system experiencing nonlinear transient motion and displayed the vast amount of results in an easily understood motion picture format - a 10 minute, 16 millimeter, color, sound motion picture supplement. An example problem with 19 mass elements in the rotor dynamics model took 0.7 second of central processing unit time per time step on an IBM 360-67 computer in a time sharing mode.

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Kascak, A. F.. 1980-01-01. Direct integration of transient rotor dynamics. https://ntrs.nasa.gov/citations/19800006869

Cite the original work for its findings. Save a collection to share your selection of sources.