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)


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    Title :

    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)


    Contributors:
    V. Esparza (author) / D. E. Thornton (author)

    Publication date :

    1976


    Size :

    435 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English