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Preliminary Results of Horizontal-Tail Load Measurements of the Bell X-5 Research Airplane
Report presenting the horizontal-tail load measurements obtained during testing of the Bell X-5 airplane at the NACA High-Speed Flight Research Station. Measurements were taken at a range of Mach numbers and from sweep angles of 20 degrees to 59 degrees.
Date:
August 15, 1952
Creator:
Rogers, John T. & Dunn, Angel H.
System:
The UNT Digital Library