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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 Bankejim.banke@nasa.govRelated Terms
Aerosciences Evaluation Test CapabilitiesHence then, the article about flight dynamics research facility characteristics was published today ( ) and is available on NASA ( Middle East ) The editorial team at PressBee has edited and verified it, and it may have been modified, fully republished, or quoted. You can read and follow the updates of this news or article from its original source.
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