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Test Summary of the Full-Span High-Lift Common Research Model at the ONERA F1 Pressurized Low-Speed Wind Tunnel

Sylvain Mouton, Grégoire Charpentier, Annabelle Lorenski

2023AIAA SCITECH 2023 Forum18 citationsDOI

Abstract

View Video Presentation: https://doi.org/10.2514/6.2023-0823.vid The main features and outcomes of the wind tunnel testing of the High-Lift Common Research Model full-span model in the ONERA F1 pressurized low-speed wind tunnel are presented. The test included variation in model configurations, angle of attack, angle of sideslip, Mach and Reynolds numbers, and included force and moment, pressure, wing deformation, and flow visualization data. The main elements of the test methodology are reviewed to better appreciate the quality of the database, in terms of uncertainty, repeatability, and wall and support corrections. A selection of results is presented regarding longitudinal and lateral characteristics, the build-up of the landing configuration, and flap setting effect.

Topics & Concepts

Wind tunnelLift (data mining)Mach numberAerodynamicsComputational fluid dynamicsStructural engineeringEngineeringTest dataAngle of attackAerospace engineeringComputer scienceData miningSoftware engineeringAerodynamics and Acoustics in Jet FlowsAerodynamics and Fluid Dynamics ResearchComputational Fluid Dynamics and Aerodynamics