CFD Aided Ship Design and Helicopter Operation

In support of Canadian industrial and defence ship design and offshore helicopter operations, a series of Ship–Helicopter Operational Limits Analysis and Simulation (SHOLAS) projects are being conducted at the National Research Council Canada (NRC) in collaboration with Defence Research and Development Canada (DRDC). This study presents a brief overview of a Canadian in-house ship airwake simulation capability combining in-house high-fidelity wind-tunnel tests, full-scale sea trials, high-order computational fluid dynamics (CFD) tools, and realistic engineering-oriented flight simulators. This paper reports challenges and lessons learned during the course of the study, discusses the current capabilities and limitations of the CFD tools and the infrastructure required, and evaluates the gaps and barriers in industry adoption by focusing on how they could be overcome based on our current practice. After validating the CFD results of an updated version of a simplified frigate shape (SFS2) and the real-world Canadian Patrol Frigate (CPF), which are in reasonable agreement with the available in-house wind-tunnel and sea-trial data, the developed approach was recently applied to the design of an undisclosed Canadian ship. Among other applications, CFD airwake results were used with confidence as input to produce representative airwake features in industrial high-fidelity piloted flight simulators.

[1]  Kévin,et al.  Turbulence characteristics of the ship air-wake with two different topside arrangements and inflow conditions , 2022, Ocean Engineering.

[2]  Richard G. Lee,et al.  Experimental investigations into the effect of at-sea conditions on ship airwake characteristics , 2022, Journal of Wind Engineering and Industrial Aerodynamics.

[3]  Ben Thornber,et al.  Quantifying uncertainty in turbulence resolving ship airwake simulations , 2021, Ocean Engineering.

[4]  I. Owen,et al.  The NATO generic destroyer – a shared geometry for collaborative research into modelling and simulation of shipboard helicopter launch and recovery , 2021 .

[5]  A. Incecik,et al.  Prediction of the aerodynamic behaviour of a full-scale naval ship in head waves using Detached Eddy Simulation , 2021 .

[6]  Ieuan Owen,et al.  Piloted Flight Simulation of Helicopter Recovery to the Queen Elizabeth Class Aircraft Carrier , 2020 .

[7]  Duan The source data , 2020 .

[8]  X. Chang,et al.  Numerical investigation of the unsteady coupling airflow impact of a full-scale warship with a helicopter during shipboard landing , 2020 .

[9]  S. Singh,et al.  Ship-helo coupled airwake aerodynamics: A comprehensive review , 2019, Progress in Aerospace Sciences.

[10]  Weixing Yuan,et al.  Combined numerical and experimental simulations of unsteady ship airwakes , 2018, Computers & Fluids.

[11]  Joseph F. Horn,et al.  Towards real-time pilot-in-the-loop CFD simulations of helicopter/ship dynamic interface , 2017, Int. J. Model. Simul. Sci. Comput..

[12]  James S. Forrest,et al.  Evaluating ship superstructure aerodynamics for maritime helicopter operations through CFD and flight simulation , 2016, The Aeronautical Journal.

[13]  Susan Polsky,et al.  Development of a Reduced Order Model to Study Rotor/Ship Aerodynamic Interaction , 2015 .

[14]  S. J. Zan,et al.  Correlated turbulence modelling: An advancing Fourier series method , 2013 .

[15]  Weixing Yuan,et al.  Simulations of Pitch–Heave Limit-Cycle Oscillations at a Transitional Reynolds Number , 2013 .

[16]  Gareth D. Padfield,et al.  Simulating the environment at the helicopter-ship dynamic interface: research, development and application , 2012, The Aeronautical Journal (1968).

[17]  Gareth D. Padfield,et al.  Ship-Helicopter Operating Limits Prediction Using Piloted Flight Simulation and Time-Accurate Airwakes , 2012 .

[18]  I. Owen,et al.  An investigation of ship airwakes using Detached-Eddy Simulation , 2010 .

[19]  Susan A. Polsky,et al.  A Computational Study of Outwash for a Helicopter Operating Near a Vertical Face with Comparison to Experimental Data , 2009 .

[20]  Susan A. Polsky,et al.  Application and verification of internal boundary conditions for antenna mast wake predictions , 2008 .

[21]  G. F. Syms,et al.  Simulation of simplified-frigate airwakes using a lattice-Boltzmann method , 2008 .

[22]  S. Polsky,et al.  Progress Towards Modeling Ship/Aircraft Dynamic Interface , 2006, 2006 HPCMP Users Group Conference (HPCMP-UGC'06).

[23]  P. Spalart,et al.  A New Version of Detached-eddy Simulation, Resistant to Ambiguous Grid Densities , 2006 .

[24]  Li Jiang,et al.  Direct numerical simulation of flow separation around a NACA 0012 airfoil , 2005 .

[25]  S. J. Zan,et al.  On Aerodynamic Modelling and Simulation of the Dynamic Interface , 2005 .

[26]  Susan A. Polsky,et al.  Application and Verification of Sub -Grid Scale Boundary Conditions for the Prediction of Antenna Wake Flowfields , 2004 .

[27]  R Spalart Philippe,et al.  Young-Person''s Guide to Detached-Eddy Simulation Grids , 2001 .

[28]  SIMULATIONS OF UNSTEADY AIRWAKES BEHIND SHIPS IN MOTION , 2018 .

[29]  Sophie Papst,et al.  Computational Methods For Fluid Dynamics , 2016 .

[30]  Richard G. Lee,et al.  A methodology to correlate simulated airwake data and unsteady helicopter load measurements to shipboard helicopter flight test data , 2015 .

[31]  Neil D. Sandham,et al.  Large Eddy Simulation of Flow Around an Airfoil Near Stall , 2010 .

[32]  S. J. Zan,et al.  Modelling and simulation of ship air wakes for helicopter operations : A collaborative venture , 1999 .