Wind-tunnel investigation at high subsonic speeds of a spoiler-slot deflector combination on an NACA 65A006 wing with quarter-chord line swept back 32.6 degrees

Vogler, Raymond D
naca-rm-l53d17
May 29, 1953


No Abstract Available

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http://naca.central.cranfield.ac.uk/reports/1953/naca-rm-l53d17.pdf