Tests were made to determine some effects of chordwise location for spoilers and blowing direction and spanwise location for jets; all controls were satisfactory roll-producing devices except canards immediately forward of main wings and spoilers at other than trailing-edge locations.
Free-flight investigation at mach numbers between 0.5 and 1.7 of zero-lift rolling effectiveness and drag of various surface, spoiler, and jet controls on 80° delta-wing missile
NASA -- Tech Note
1960
47 pages
Report
Englisch
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