Wind-tunnel investigation of the aerodynamic characteristics of a one-fifteenth-scale model of the Northrop MX-775A missile

E. Ray Phelps, Frank A. Lazzeroni
naca-rm-a51e28
Oct 1951


This report presents the results of a wind-tunnel investigation conducted to determine the control effectiveness and the variations of forces and moments as functions of angles of attack and sideslip for a one-fifteenth-scale model of the MX-775 missile. The major portion of the data presented is for Mach numbers of 0.85, 0.92, 1.30, 1.40, and 1.70 at a Reynolds number of 2.20 million.

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http://naca.central.cranfield.ac.uk/reports/1951/naca-rm-a51e28.pdf