The Open-Source Offshore (OSO) airfoils have been created by Sandia National Laboratories (SNL) and the National Renewable Energy Laboratory (NREL) to meet modern design criteria for offshore wind turbines without proprietary constraints. Targeting the IEA 22 MW wind turbine, the OSO-21-WT1 and OSO-30-WT1 airfoils were designed through feedback from industry experts and advanced analysis tools. While most performance metrics were achieved, the OSO-21-WT1 exceeded the roughness loss metric and both airfoils moderately exceeded the desired lift coefficient margin. Detailed design criteria and computed metrics are available, indicating successful structural performance compared to existing airfoils. The airfoil data will be publicly accessible via SNL’s GitHub repository. This initiative aims to enhance research and development in offshore wind technology while fostering collaboration among federal laboratories, academic institutions, and industry stakeholders, facilitating advancements in renewable energy solutions.

This document provides information on test planning for high-Reynolds number airfoil evaluations at the National Full-Scale Aerodynamics Complex (NFAC). It outlines the measurement and diagnostic equipment necessary for accurate aerodynamic testing, including force, pressure, velocity, and temperature measurements using tools such as loads balances, strain gauges, pressure rakes, hot wire systems, and infrared thermography. Additionally, it presents preliminary cost estimates for fabricating a test model, which is approximately 10 meters by 3 meters in size, with total costs ranging from $500,000 to $600,000. The breakdown includes expenses for a conventionally constructed model and additional costs for facility integration and instrumentation hardware. The document notes that utilizing 3D printing could reduce fabrication costs. Overall, the document serves as a technical reference for stakeholders involved in aerodynamic testing and funding applications, ensuring they are informed about necessary resources, expected costs, and measurement technologies essential for successful project execution in the context of government RFPs and grants.

The document outlines a comprehensive cost estimate for conducting high Reynolds number tests at the NASA Ames Research Center's National Full-Scale Aerodynamics Complex (NFAC) scheduled for March 2025. The total baseline test cost is projected at $3,078,742, which includes various components such as planning, installation, operations, and removal. Detailed costs for each operational phase are provided, with additional NASA support costs and specialized instrumentation factored in. The report highlights the need for funds to be secured before test execution and notes that actual costs may vary from estimates. The document emphasizes the careful planning required to ensure efficient operations, including electrical power usage, which is dependent on run conditions. Overall, the estimate serves as a critical element for securing federal funding while supporting the Department of Energy's goals for advanced aerodynamics research. The detailed financial breakdown demonstrates the project's complexity and underscores the importance of accurate cost forecasting in government RFP processes.

The National Full-Scale Aerodynamics Complex (NFAC) Test Planning Guide outlines the procedures for conducting experiments in its 40x80 and 80x120 feet wind tunnels. Managed by the U.S. Air Force's Arnold Engineering Development Complex, the guide offers critical information for customers preparing tests, ensuring safety, and efficient execution. It details the test process, which includes the planning phase, design and fabrication, test execution, and reporting. Each phase demands careful coordination and a rigorous documentation process, emphasizing safety, analytical analysis, and customer collaboration. Significant focal points include the required documentation for planning tests, instrumentation specifications, system safety analyses, and customer equipment integration procedures. The guide mandates compliance with safety regulations and specifies that detailed analysis of the test article's structural integrity must be provided by the customer. Moreover, it establishes timelines for document submissions and operational readiness reviews, highlighting the importance of timely communication to prevent project delays. This guide serves as a comprehensive reference for both government and commercial agencies involved in aerodynamics testing, reflecting NFAC's commitment to high standards in research and development, while ensuring personnel safety and operational efficacy.

The Aerodynamics for Large Turbines (ALTius) project focuses on addressing the aerodynamic performance knowledge gap for modern offshore wind turbines over 10 MW. As turbine designs scale up, existing aerodynamic model data is insufficient, particularly for high Reynolds number (over 25 million) conditions that significantly influence performance and structural integrity. The objective is to collect and analyze high-quality aerodynamic data for airfoils operating in this range, aiming to improve predictive models. The project includes extensive wind tunnel testing at the National Full-Scale Aerodynamics Complex (NFAC) to gather specific performance measurements, such as lift and drag coefficients and flow characteristics. Key deliverables include comprehensive datasets made publicly available to support research and development within the wind energy sector. The work also involves close collaboration between subcontractors and NFAC for airfoil selection, test execution, data analysis, and compliance with safety and design specifications. Overall, the effort aims to enhance the understanding and performance evaluation of large wind turbine aerodynamics, ultimately contributing to the advancement of wind energy technologies.

The document outlines a Request for Proposal (RFP) for the aerodynamic characterization of nonoperational load phenomena in wind turbines. It emphasizes the importance of accurately modeling and simulating the aerodynamic loads and vibrations that blades experience during idle, maintenance, or adverse weather conditions. The objective is to gather and validate benchmark aerodynamic data to improve wind turbine design tools, ultimately leading to more cost-effective technology in the wind energy sector. Key tasks include conducting wind tunnel experiments to assess 3D unsteady aerodynamics, instrumenting blade articles under various flow conditions, and developing test plans that meet specified Reynolds number criteria. The project requires regular progress reporting, reviews, and collaborative meetings with NREL and WETO teams. All data collected will be publicly available, and proprietary data will have limited access for research purposes. The deliverables outlined include various reports, test data documentation, and validation results aimed at enhancing the understanding of nonoperational turbine behaviors and reducing financial risks associated with innovation in wind energy technology. The overarching aim is to accelerate the development of wind energy capabilities and ensure the safety and reliability of large wind turbine operations.

The subcontract between the Alliance for Sustainable Energy, LLC, and a yet-to-be-named subcontractor is established to fulfill obligations of the Prime Contract with the Department of Energy (DOE) for managing the National Renewable Energy Laboratory (NREL). The document outlines the scope of work, payment terms, and compliance policies. The subcontractor is to perform tasks detailed in Appendix A, with payment contingent upon the acceptance of specified deliverables. It emphasizes the need for adherence to export control laws and addresses the submission of invoices and reporting requirements to facilitate payment. The subcontract also contains provisions for scientific integrity, ensuring that all parties maintain transparency and uphold research standards. It stipulates the rights to proposal data and outlines the process for releasing public information regarding the work conducted. Compliance with federal regulations regarding foreign government affiliations and activities is highlighted, emphasizing the need for subcontractor personnel to disclose any participation in such programs. Overall, the document aims to establish clear expectations and guidelines for successfully executing projects under this subcontract, ensuring accountability and adherence to federal standards.

The government document outlines a comprehensive Deliverable Summary Table related to high-Reynolds number airfoil aerodynamics and aerodynamic characterization of non-operational loads phenomena. It specifies key tasks and deliverables, including quarterly progress reports, design and science plans, test article fabrication, and validation data delivery. Each scheduled task is categorized by its occurrence, with notes indicating that offerors can modify the deliverables as necessary while maintaining the minimum requirements. The document serves as a guide for potential offerors to structure their project proposals, emphasizing collaboration with National Full-Scale Aerodynamics Complex (NFAC) and the National Renewable Energy Laboratory (NREL). The focus is on achieving high-quality testing and validation data to support ongoing research and development in aerodynamics, ensuring deliverables support project management effectively. The inclusion of regular progress reports and technical reviews indicates a structured approach to project execution, facilitating knowledge sharing and lessons learned throughout the process. This summary is crucial for understanding the requirements and expectations for proposals in government-funded aerodynamics research.

The National Renewable Energy Laboratory (NREL) is soliciting proposals for the RFP RFX-2025-10021 titled "Fundamental Aerodynamics for Large Wind Turbine Performance and Reliability." This initiative aims to address knowledge gaps in aerodynamic data for large wind turbines, specifically regarding airfoil performance and nonoperational loads. The RFP seeks innovative approaches to collect benchmark aerodynamic data and improve modeling tools, essential for the design and reliability of next-generation turbines. Proposal submissions are divided into two topic areas: the collection of high Reynolds number airfoil data and the characterization of aerodynamic loads during nonoperational conditions. Eligible participants include domestic entities like educational institutions and for-profit organizations, with a focus on performance conducted entirely within the United States. Evaluation criteria emphasize technical merit, project approach, and team capabilities, with a competitive range structured under a Best Value Selection process. The estimated budget for Topic Area 1 is $4.75 million and $1.5 million for Topic Area 2, requiring a minimum price participation from offerors, except for educational and nonprofit organizations. The project period is anticipated to last up to 36 months, highlighting the U.S. commitment to advancing sustainable wind energy technology.