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.

Personal Author(s):

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

Subject Categories:

File Size:

0.00MB

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