The results are presented of a force test of a .88 percent scale model of the 142 inch solid rocket booster without protuberances, conducted in the MSFC high Reynolds number wind tunnel. The objective of this test was to obtain aerodynamic force data over a large range of Reynolds numbers. The test was conducted over a Mach number range from 0.4 to 3.5. Reynolds numbers based on model diameter (1.25 inches) ranged from .75 million to 13.5 million. The angle of attack range was from 35 to 145 degrees. (Author)
Force Test of a 0.88 Percent Scale 142-Inch Diameter Solid Rocket Booster (MSFC Model Number 461) in the NASA/MSFC High Reynolds Number Wind Tunnel (SAL3F)
1976
193 pages
Report
Keine Angabe
Englisch
Uncertainty Analysis of the NASA MSFC 14-Inch Trisonic Wind Tunnel
British Library Conference Proceedings | 1999
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