As discussed in our previous articles, regulatory pressure, advances in wind technology including cost acquisition reduction and rising fuel costs are driving the adoption of Wind-Assisted Ship Propulsion (WASP) technologies as a key decarbonization pathway. However, as the number of systems and stakeholders increases, so does the complexity of the language used.
Today, different actors such as naval architects, regulators, shipowners and technology providers, often use different terms to describe the same concepts, or the same terms with different meanings. This lack of standardization leads to confusion, hinders fair comparisons, and slows down investment decisions.
Organizations like IMO, ITTC, and IWSA have made significant progress in developing common definitions and technical guidelines (e.g., IMO Circ.896, ITTC Recommended Procedures 2024, IWSA White Paper). This article builds on those efforts to introduce key concepts and vocabulary, helping readers navigate the language of today’s wind propulsion landscape.
At the core of wind propulsion lies a simple physical principle: when air flows around a surface, a pressure difference is generated, creating an aerodynamic force. This force can be decomposed into lift (perpendicular to the flow) and drag (parallel to the flow). By properly orienting and trimming wind propulsion devices, the lift vector can be directed to produce thrust in the vessel’s direction of travel (driving force), thereby reducing the load on the main engine.
In traditional sailing, sails are adjusted to exploit the incoming wind, generating forward thrust. Modern Wind-Assisted Ship Propulsion (WASP) devices rely on the same aerodynamic fundamentals but use engineered geometries: rigid wings, flettner rotors, suction sails or kites that are optimized for performance, durability, and integration with large commercial vessels. The fundamental aerodynamic relationship is:

where L is the lift force, D is the drag force, ρ is air density, V is the relative wind speed and S is the device’s projected surface area. CL is the lift coefficient and CD is the drag coefficient of the selected device, and each WASP device will offer different aerodynamic coefficients depending on its geometry and operating conditions.
To integrate these forces into ship performance, the thrust (CT) and side or heeling force (CH) coefficients are used, linking the aerodynamic forces to the vessel’s hydrodynamics. The ship must balance these forces through leeway, heel, and rudder (plus additional appendages) action to maintain course. This interaction explains why installation layout, position relative to superstructure, and multi-device interference are critical in performance prediction.
Finally, performance is often summarized using polar diagrams, circular plots showing thrust, power, or savings across true wind speeds and angles. These diagrams illustrate how different device types behave under varying conditions and are fundamental inputs for route simulations and operational performance assessments.
Traditionally, sailing performance has been represented through CL — CD polars, which plot the lift coefficient (CL) against the drag coefficient (CD) for different angles of attack. These curves illustrate how efficiently a device converts wind energy into useful lift across a range of aerodynamic settings.
On a CL — CD polar plot, each point on the curve corresponds to a specific angle of attack, and the straight line drawn from the origin to that point represents the total aerodynamic force vector FA for that setting. The angle β represents the apparent wind angle.
For a given apparent wind angle, the maximum propulsive force can be found graphically. This is done by drawing a line with a direction perpendicular to the vessel’s course and shifting it until it becomes tangent to the polar curve. The point of tangency represents the optimal sail or device trim for that wind angle, the condition where the driving force (aligned with the ship’s course) is maximized. Decomposing the total aerodynamic force at this point gives two components: the driving force (T), which contributes to propulsion, and the side force (SA) which causes heeling and must be balanced by the vessel’s hydrodynamics.
This is the fundamental aerodynamic “potential” of the device, independent of ship dynamics, and each wind propulsion device has its own polar shape depending on its aerodynamic characteristics. However, ships operate within complex hydrodynamic environments. So, once aerodynamic forces are computed, they are embedded into Velocity Prediction Programs (VPPs) that solve the force equilibrium between wind propulsion devices and the vessel’s hydrodynamics across a range of Apparent Wind Angles (AWA) and speeds.
The result is a ship polar diagram, a circular plot that shows thrust, power, or fuel savings at different True Wind Angles (TWA) and wind speeds for a given ship speed. VPP programs not only solve for the force equilibrium, but also optimize the overall performance of the ship, so each point on a ship polar diagram considers the best trimming condition for the aerodynamic devices.
Main Types of Wind Propulsion Systems
Modern Wind-Assisted Ship Propulsion (WASP) technologies are based on the same aerodynamic principles but differ widely in geometry, control systems, and integration complexity. They can be broadly grouped into six main categories: soft sails, hard sails or wingsails, Flettner rotors, suction wings, kites, and hull form adaptations.
Each system generates thrust through the interaction of lift and drag forces, but the way these forces are produced and controlled defines their efficiency, power demand, and operational use. At the end, each technology presents distinct trade-offs in terms of aerodynamic efficiency, control complexity, and integration feasibility. The choice of system ultimately depends on vessel type, operational profile, and desired balance between capital investment, energy savings, and regulatory compliance.
It is important to note that the CL and CD values presented here are indicative and serve only as references to illustrate the aerodynamic potential and behavior of each device type. Actual coefficients depend strongly on each system’s geometry, control strategy, and trim configuration, meaning that accurate performance estimation requires device-specific analysis under representative operating conditions.
Their aerodynamic efficiency depends on sail tension and form stability, with typical lift coefficients (CL) between 1.0 and 1.5, and drag coefficients (CD) between 0.05 and 0.2. Although they require little to no electrical power, only limited energy for trimming.
New materials and production techniques are increasing the soft sails categories. Now these sails come in a wide variety of configurations and shapes, like the dynarig system, hybrid designs using furlable rigid panels or inflatable sail systems. The sizes for these types of sails vary considerably and will depend on stability and maximum heeling moment factors.
The resulting high aerodynamic efficiency enables strong upwind capability and steady performance across a wide range of wind angles. Power needs are minimal, typically a few kilowatts per unit, limited to automatic control and positioning systems. Commercial sizes vary from ~9 m to 40 m in height, depending on vessel size and route.
Flettner rotors can achieve remarkably high lift coefficients (CL= 5–10) with moderate drag (CD ≈ 3–4) at high spin ratio values. Instead of angle of attack, the main parameter affecting aerodynamic efficiency is the spin ratio, the ratio of cylinder surface speed to wind speed. Aspect ratio (height/diameter) and end-plate ratio are also critical parameters in maximizing efficiency, and some manufacturers offer hydraulic tilting or folding mechanisms that allow the rotor to lie horizontally during cargo handling or under bridges.
They require continuous electric power, typically between 40 and 115 kW per rotor at maximum RPM, but their net energy gain far exceeds consumption under favorable conditions. Commercial sizes vary from ~18 to 35 m in height and 3 to 5 m in diameter.
This active boundary-layer control allows for much higher lift at large angles of attack, with CL values up to 6–8 and CD values between 1.5 and 3, at same operational conditions. Their performance will depend on the ventilation power (or suction coefficient), the effectiveness of boundary layer suction and the angle of attack.
Power consumption remains moderate (typically below 15 kW per unit), making them an attractive option for vessels seeking a balance between efficiency and simplicity. Commercial sizes vary from ~12 m to 36 m in height.
The CLmax at useful operating AoA for modern towing kites lies between 1.0 –1.5. The associated CD at those “best glide / best tow” points fall roughly 0.2–0.3, yielding L/D ~3–7 for contemporary systems. Kites are particularly effective on ocean routes with consistent wind conditions, offering strong performance in downwind conditions without adding drag to the vessel structure when retracted. Sizes can vary depending on many factors, ranging from 500 to 1000 m2.
With the fundamentals established; to help navigate this technical and regulatory landscape, we’ve compiled a glossary of essential terms used across the wind propulsion industry. The terms are grouped by theme. (All definitions adapted from IMO, ITTC, IWSA White Paper, Wind Propulsion Principles and internal work).
As wind propulsion enters mainstream shipping, a shared vocabulary is becoming a necessity. Clear, consistent terminology enables fair comparisons, supports regulatory alignment, and accelerates market adoption. This article has introduced the core aerodynamic principles, main system types, and key terms used across the sector, drawing from IMO, ITTC, and IWSA definitions.
These concepts underpin the technical, regulatory, and business conversations shaping the future of wind propulsion. As the industry advances toward 2030, 2040, and 2050 decarbonization checkpoints, alignment in language will be as vital as alignment in strategy. Only through common understanding can we ensure that technical innovation, regulatory recognition, and market adoption move in the same direction, with the wind.
References
During the 33rd America’s Cup cycle, Mario Caponnetto contributed to hydrodynamic assessment workstreams aligned with the BMW Oracle wing-sail platform, the configuration that ultimately won the Match. This milestone marked the shift toward aero-hydrodynamic integration in Cup design culture.
BMW Oracle Racing
America’s Cup / Aero-Hydro Integration / Performance Engineering
In 2021, Caponnetto Hueber led the CFD, foil design, and hydrodynamic engineering for the AC75 of Luna Rossa Challenge, the eventual Prada Cup winner. We deployed multiscale CFD and aero-hydro coupling to ensure optimum lift and control. Rapid iteration delivered performance gains under tight competition timelines.
Luna Rossa Challenge
Racing Concept / CFD / Foil Design