Aerodynamic Control Effectiveness of a Cruciform Trailing Edge Controlled Vehicle at High Subsonic Mach Numbers Using Individual Flap Effectiveness. Book 2.
Final rept. Oct 73-Apr 74,
AIR FORCE ARMAMENT LAB EGLIN AFB FL
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This report documents the technique and results of describing the aerodynamic control effectiveness of a cruciform trailing edge controlled vehicle using the effectiveness of each of the four control surfaces. This report consists of two books of which this is Book 2 containing Appendixes G to L.
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