NASA NTRS · 19810000075
Aeroelastic Analysis for Rotorcraft
Abstract
Aeroelastic-analysis computer program incorporates an analytical model of aeroelastic behavior of wide range of rotorcraft. Such an analytical model is desirable for both pretest predictions and posttest correlations. Program can be applied in investigations of isolated rotor aeroelasticity and helicopter-flight dynamics and could be employed as basis for more-extensive investigations or aeroelastic behavior, such as automatic control system design.
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Johnson, W.. 1982-09-01. Aeroelastic Analysis for Rotorcraft. https://ntrs.nasa.gov/citations/19810000075
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