Results are presented of a 0.10 scale orbiter forebody test with left and right mounted air data probes (ADP) as well as a flight test probe (nose boom). Left and right ADP data were obtained at Mach numbers of .3, .4, .5, .6, .7, .8, .85, .9, .95, .98, 1.05 and 1.1 through a Reynolds number range of 1.3 to 4.4 million. Nose boom data were obtained at Mach numbers of .3, .4, .5, .6, .7, .9 and .98. (Author)
Results of an Air Data Probe Investigation Utilizing a 0.10 Scale Orbiter Forebody (Model 57-0) in the Ames Research Center 14-Foot Wind Tunnel (OA220)
1976
435 pages
Report
Keine Angabe
Englisch