NASA NTRS · 19890000377
Predicting Flutter Of A Propfan
Abstract
Report discusses theoretical model and associated computer program for prediction of subsonic bending-torsion cascade flutter in propfans. Predictions of model compared with results of experiments. Additional parametric studies illustrate effects upon flutter speed of steady aeroelastic deformations, angle at which blade set, speed of rotation, structural damping, and number of vibrational modes. Calculations performed by parts of ASTROP computer code: ASTROP 2, based on two-dimensional, subsonic, unsteady aerodynamics; and ASTROP 3, based on three-dimensional, subsonic, steady and unsteady aerodynamics.
Keep this discovery
Explore connections, maps & timelines
Kaza, K. R. V., Mehmed, O., Narayanan, G. V., Murthy, D. V.. 1989-07-01. Predicting Flutter Of A Propfan. https://ntrs.nasa.gov/citations/19890000377
Cite the original work for its findings. Save a collection to share your selection of sources.