Three-Component Force Measurements for Scramjet Engines 1) Engine Drag from Mach 4 to Mach 8 Flight Conditions
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Pressure Measurements on a Slender Rhombic Cone at Incidence at Mach Numbers from 0-4 to 1-1
Pressures have been measured on a wing in the form ofa rhombic cone at two cross-sections and along a single generator. The wing had an aspect ratio of one and a leading-edge angle of 60 °. Measurements were made at M = 0.4, 0.6, 0.82, 0.9, 1.0 and 1.1, at angles of incidence up to 20 ° and at a Reynolds number of 6 million, based on model length. At the lowest Mach number the tests were repeat...
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ژورنال
عنوان ژورنال: JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
سال: 2003
ISSN: 1344-6460
DOI: 10.2322/jjsass.51.244