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Flight Dynamics Research Facility Characteristics

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    The Flight Dynamics Research Facility (FDRF) is a large, subsonic wind tunnel with a vertical test section for conducting flight dynamics research for stability, controllability, free-fall and aircraft spin, and spin recovery testing of atmospheric vehicles.

    Characteristics

    Test Section Dimensions: 20 ft. diam. by 24 ft. high Speed: 0 – 172 ft/s (0 – 117 mph) Dynamic Pressure: (0 – 35 psf) Reynolds Number: 0 – 1.10×10^6 per ft. Pressure: Atmospheric Temperature: Actively cooled (79° F) Test Gas: Air Facility Height: 131 ft.

    Flight Dynamics Flight Research

    Aerosciences Evaluation and Test Capabilities

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    Last Updated Jun 09, 2026 EditorLillian GipsonContactJim [email protected]

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    Aerosciences Evaluation Test Capabilities

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