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- W2738852019 abstract "Experimental data from wind-tunnel tests of the Rigid Semispan Model (RSM) performed a_ NASA Langley's Transonic Dynamics Tunnel (TDT) are presented. The primary focus of the paper is on da_a obtained from testing of the RSM on the Oscilla_ing Turntable (OTT). The OTT is capable of oscillating models in pitch at various amplitudes and frequencies about mean angles of attack. Steady and unsteady pressure data obtained during testing of the RSM on the OTT is presented and compared to data obtained from previous tests of the RSM on a load balance and on a Pitch and Plunge Apparatus (PAPA). Testing of _he RSM on the PAPA resulted in flutter boundaries that were strongly dependent on angle of attack across the Mach number range. Pressure data from all three tests indicates the existence of vortical flows at moderate angles of attack. The correlation between the vortical flows and the unusual flutter boundaries from the RSM/PAPA test is discussed. Comparisons of experimental data with analyses using the CFL3Dv6 computational fluid dynamics code are presented." @default.
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- W2738852019 date "2002-01-01" @default.
- W2738852019 modified "2023-09-27" @default.
- W2738852019 title "of Unsteady Pressure Data on a Large HSCT Semispan Wing and Comparison with Analysis" @default.
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