NATO RTO AVT Task Group-080 "Vortex Breakdown over Slender Wings": Objectives and Overview

The paper will present the framework of fully automated two/three dimensional ice accretion simulation package NSMB3D-ICE, with emphasis on the remeshing step. The NSMB3D-ICE Navier-Stokes code, coupled to an Eulerian droplet module and iterative Messinger thermodynamic model, can perform multi time-steps ice accretion simulations via an automated multi-block elliptic/parabolic grid generation code (NSGRID3D). Attention is paid to the efficiency and robustness of the numerical procedure especially for complex 3D glaze ice simulation. The new automated multi time-step icing code NSMB3D-ICE/NSGRID3D is validated and verified using several icing case studies such as the GLC305-3D rime and glaze ice cases.

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NATO RTO AVT Task Group-080 "Vortex Breakdown over Slender Wings": Objectives and Overview

Cited by 2 publications

References 18 publications

NATO RTO AVT Task Group-080 "Vortex Breakdown over Slender Wings" Validation and Verification, Conclusions and Recommendations

NATO RTO AVT Task Group-080 "Vortex Breakdown over Slender Wings" Validation and Verification, Conclusions and Recommendations

Multi-time Step Icing Calculations Using a 3D Multi-block Structured Mesh Generation Procedure

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