AERODYNAMIC RESULTS OS A SEPARATION TEST (CA20) CONDUCTED AT BOEING TRANSONIC WIND TUNNEL USING 0.03-SCALE MODELS OF THE CONFIGURATION 140A/B (MODIFIED) SSV ORRIER SSV ORBITER (MODEL No. 45-0) AND THE BOEING 747 CARRIER (MODEL NO. AX 1319 X-1)

摘要

In addition to the balance force data, pressures were measured. Pressure edifices were located at the nose of the Orbiter, on either side of the vertical bade strut, and at the mid-root chord on either side of the vertical tail. Strain goes were installed on the Basing 747 vertical tail to in dictate buffet inset.