Aerodynamic modelling of fin stabilised underslung loads

K. Enciu, A. Rosen

Research output: Contribution to journalArticle

5 Scopus citations

Abstract

Box-like slung loads exhibit periodic yaw response instabilities, while carried externally by a helicopter. When coupled with the slung load longitudinal and lateral pendulum motions, these instabilities result in significant pendulum oscillations of the load. High amplitude oscillations lead in many cases to the limiting of a load's flight envelope. Using wind tunnel and flight tests, rear mounted fins were previously demonstrated as efficient means for stabilisation of a problematic load. However, the lack of a proper analytical model of the stabilised load's aerodynamic characteristics, led to a trial and error development process, without an appropriate physical understanding of the stabilisation problem. The present paper describes a method for the aerodynamic modeling of fins stabilised slung loads based on a limited number of simple static wind-tunnel tests. The resulting database is incorporated in a dynamical slung load simulation that shows good agreement with dynamic wind-tunnel tests. The applicability of the proposed method is demonstrated, by the calculation of stabilised loads aerodynamic databases for interim fn inclination angles not covered by tests.

Original languageEnglish (US)
Pages (from-to)1073-1103
Number of pages31
JournalAeronautical Journal
Volume119
Issue number1219
DOIs
StatePublished - Sep 1 2015

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

Fingerprint Dive into the research topics of 'Aerodynamic modelling of fin stabilised underslung loads'. Together they form a unique fingerprint.

  • Cite this