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- W16483684 abstract "A numerical finite-difference procedure has been developed for the modeling of rotor self-generated blade-vortex interactions (BVI). The interaction velocity field is obtained through a nonlinear superposition of the rotor and the vortex wake flow fields. Vortex effects are simulated using the velocity 'transpiration' approach. Potential blade-vortex encounters are identified and tracked in time at equal increments of rotor azimuth using the lifting-line helicopter/rotor trim code CAMRAD. Accuracy of the numerical results were found to rely heavily on the CAMRAD-predicted vortex orientation, vortex strength, and user specified vortex core radius. Results for the subcritical self-generated BVI for the model OLS rotor are presented. They show good agreement with the experimental wind tunnel data." @default.
- W16483684 created "2016-06-24" @default.
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- W16483684 date "1990-01-01" @default.
- W16483684 modified "2023-09-27" @default.
- W16483684 title "Finite-difference solutions of three-dimensional rotor blade-vortex interactions" @default.
- W16483684 hasPublicationYear "1990" @default.
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