Flight investigation to determine lift and drag characteristics of a canard ram-jet missile configuration in the Mach number range of 0.8 to 2.0

Gammal, Abraham A Kennedy, Thomas L
naca-rm-l54d28
June 17, 1954


No Abstract Available

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http://naca.central.cranfield.ac.uk/reports/1954/naca-rm-l54d28.pdf