1. Reference 1 documents tests performed at the supersonic wind tunnel of the Naval Surface Weapons Center Laboratory at White Oak, Maryland. The tests were performed at Mach numbers 3.5, 4.0 and 5.0, with the majority of tests being run at M = 5.0 . The Reynolds number for the tests varied between 4.0 through 5.8 x lo 6 per foot (12.2-19.0 x lo 6 per meter).