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Flight-Measured Aerodynamic Loads on a 0.92 Aspect Ratio Lifting Surface (1978)

Meyer, R. R., Jr. ; Deangelis, V. M.

In: CASI

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Publication Date: 2016-06-07

Description: Ventral fin loads, expressed as normal force coefficients, bending moment coefficients, and torque coefficients, were measured during flight tests of a YF-12A airplane. Because of the proximity of the ventral fin to the ailerons, the aerodynamic loads presented were the result of both sideslip loads and aileron crossflow loads. Aerodynamic data obtained from strain gage loads instrumentation and some flight pressure measurements are presented for several Mach numbers ranging from 0.70 to 2.00. Selected wind tunnel data and results of linear theoretical aerodynamic calculations are presented for comparison.

Keywords: AERODYNAMICS

Type: YF-12 Experiments Symp., Vol. 1; p 73-91

Format: application/pdf

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