Drag characteristics of rectangular and swept-back NACA 65-009 airfoils having aspect ratios of 1.5 and 2.7 as determined by flight tests at supersonic speeds

Alexander, Sidney R Katz, Ellis
naca-rm-l6j16
February 24, 1947

No Abstract Available

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http://naca.central.cranfield.ac.uk/reports/1947/naca-rm-l6j16.pdf