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Accession Number:
AD0919646
Title:
Aerodynamic Control Effectiveness of a Cruciform Trailing Edge Controlled Vehicle at High Subsonic Mach Numbers Using Individual Flap Effectiveness. Book 2.
Descriptive Note:
Final rept. Oct 73-Apr 74,
Corporate Author:
AIR FORCE ARMAMENT LAB EGLIN AFB FL
Report Date:
1974-04-01
Pagination or Media Count:
263.0
Abstract:
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.
Distribution Statement:
APPROVED FOR PUBLIC RELEASE