Abstract
Flights of rotorcraft over the desert floor can result in significant entrainment of particulate matter into the atmospheric boundary layer. Continuous or widespread operation can lead to local and regional impacts on visibility and air quality. To account for this pollutant source in air quality models, a parameterization scheme is needed that addresses the complex vertical distribution of dust ejected from the rotorcraft wake into the atmospheric surface layer. A method to parameterize the wind and turbulence fields and shear stress at the ground is proposed here utilizing computational fluid dynamics and a parameterized rotor model. Measurements taken from a full scale experiment of rotorcraft flight near the surface are compared to the simulation results in a qualitative manner. The simulation is shown to adequately predict the forward detachment length of the induced ground jet compared to the measured detachment lengths. However, the simulated ground vortex widths and vorticity deviate substantially from the measured values under a range of flight speeds. Results show that the method may be applicable for air quality modeling assuming slow airspeeds of the rotorcraft, with advance ratios of 0.005–0.02.
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Abbreviations
- ASL:
-
Atmospheric surface layer
- CFD:
-
Computational fluid dynamics
- DRI:
-
Desert Research Institute (Nevada)
- M-O:
-
Monin-Obukhov
- RANS:
-
Reynolds Averaged Navier-Stokes
- TKE:
-
Turbulent kinetic energy
- VBM:
-
Virtual Blade Model
- VTM:
-
Vorticity Transport Model
- YPG:
-
Yuma Proving Grounds
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McAlpine, J.D., Koracin, D.R., Boyle, D.P. et al. Development of a rotorcraft dust-emission parameterization using a CFD model. Environ Fluid Mech 10, 691–710 (2010). https://doi.org/10.1007/s10652-010-9191-y
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DOI: https://doi.org/10.1007/s10652-010-9191-y