NASA NTRS · 19930051990
Helicopter response to atmospheric turbulence
Abstract
A new time-domain method for simulating cyclostationary turbulence as seen by a translating and rotating blade element has recently been developed for the case of one-dimensional spectral distribution. This paper extends the simulation method to the cases of two- and three-dimensional spectral distributions and presents validation results for the two-dimensional case. The statistics of an isolated rigid blade flapping response to turbulence are computed using a two-dimensional spectral representation of the von Karman turbulence model, and the results are compared with those obtained using the conventional space-fixed turbulence analysis. The new turbulence simulation method is used for predicting the Black Hawk helicopter response to atmospheric turbulence.
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Riaz, J., Prasad, J. V. R., Schrage, D. P., Gaonkar, G. H.. 1992-01-01. Helicopter response to atmospheric turbulence. https://ntrs.nasa.gov/citations/19930051990
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