Dynamics of a slung load

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Abstract

The yaw damping coefficient of an 8 × 8 × 20 ft cargo container is experimentally determined by forced oscillation tests. The result is then used in linearized small-perturbation stability analyses of a slung load, considering both single-cable and two-cable tandem suspension systems. The effect of attaching stabilizing fins to the container and of incorporating a rotating wheel for stability augmentation is also theoretically investigated. The results agree well with previous model and full-scale tests and also show that the two-cable tandem suspension system may offer a satisfactory means of transporting the standard cargo container throughout the speed range of most present-day cargo helicopters. © 1977, American Institute of Aeronautics and Astronautics, Inc. All rights reserved.

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APA

Feaster, L., Poli, C., & Kirchhof, R. (1977). Dynamics of a slung load. Journal of Aircraft, 14(2), 115–121. https://doi.org/10.2514/3.44578

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