DID YOU KNOW? DTIC has over 3.5 million final reports on DoD funded research, development, test, and evaluation activities available to our registered users. Click
HERE to register or log in.
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.
Corporate Author:
AIR FORCE ARMAMENT LAB EGLIN AFB FL
Report Date:
1974-04-01
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.
Descriptive Note:
Final rept. Oct 73-Apr 74,
Supplementary Note:
See also Book 1, AD-919 645L.
Pages:
0263
File Size:
0.00MB
