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

Personal Author(s):

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.

Subject Categories:

  • Guided Missiles
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE