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Eulerian simulation of the fluid dynamics of helicopter brownout

Phillips, C. and Brown, R.E. (2009) Eulerian simulation of the fluid dynamics of helicopter brownout. Journal of Aircraft, 46 (4). pp. 1416-1429. ISSN 0021-8669

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      Abstract

      A computational model is presented that can be used to simulate the development of the dust cloud that can be entrained into the air when a helicopter is operated close to the ground in desert or dusty conditions. The physics of this problem, and the associated pathological condition known as 'brownout' where the pilot loses situational awareness as a result of his vision being occluded by dust suspended in the flow around the helicopter, is acknowledged to be very complex. The approach advocated here involves an approximation to the full dynamics of the coupled particulate-air system. Away from the ground, the model assumes that the suspended particles remain in near equilibrium under the action of aerodynamic forces. Close to the ground, this model is replaced by an algebraic sublayer model for the saltation and entrainment process. The origin of the model in the statistical mechanics of a distribution of particles governed by aerodynamic forces allows the validity of the method to be evaluated in context by comparing the physical properties of the suspended particulates to the local properties of the flow field surrounding the helicopter. The model applies in the Eulerian frame of reference of most conventional Computational Fluid Dynamics codes and has been coupled with Brown's Vorticity Transport Model. Verification of the predictions of the coupled model against experimental data for particulate entrainment and transport in the flow around a model rotor are encouraging. An application of the coupled model to analyzing the differences in the geometry and extent of the dust clouds that are produced by single main rotor and tandem-rotor configurations as they decelerate to land has shown that the location of the ground vortex and the size of any regions of recirculatory flow, should they exist, play a primary role in governing the extent of the dust cloud that is created by the helicopter.

      Item type: Article
      ID code: 27438
      Notes: Also presented at: 64th American Helicopter Society Annual Forum (2008). This is a variant record V: 27501
      Keywords: eulerian simulation, fluid dynamics, helicopter brownout, aerodynamic forces, vorticity transport model, Mechanical engineering and machinery, Motor vehicles. Aeronautics. Astronautics, Aerospace Engineering
      Subjects: Technology > Mechanical engineering and machinery
      Technology > Motor vehicles. Aeronautics. Astronautics
      Department: Faculty of Engineering > Mechanical and Aerospace Engineering
      Related URLs:
      Depositing user: Ms Katrina May
      Date Deposited: 13 Sep 2010 15:26
      Last modified: 09 Sep 2014 09:27
      URI: http://strathprints.strath.ac.uk/id/eprint/27438

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