WIND TUNNEL TESTS OF AN 0.015-SCALE CONFIGURATION 140A/B SPACE SHUTTLE ORBITER MODEL (67-0) IN THE NASA/LRC 8-FOOT TPT TO OBTAIN TRANSONIC AERODYNAMIC FORCE DATA (OA106)

摘要

This report contains the results of wind tunnel tests of the NASA/ Rockwell 0.015-scale Configuration 4 (140A/B) Orbiter model (67-0).nThese tests were conducted to obtain longitudinal stability a control data for Hach numbers from 0.35 to 1.2. Data were obtained for an alpha range of -2° to +22° at beta = 0°.nThe effect of speed brake deflection and body flap deflection was obtained through the Hach range. Boundary layer transition strips were used on the model.