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):

• Rogers, Robert M.

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.

Descriptors:

• *GUIDED MISSILES
• *TRAILING CONTROL SURFACES
• *CRUCIFORM WINGS
• TRAILING EDGES
• MATHEMATICAL MODELS
• EXPERIMENTAL DATA
• MACH NUMBER
• FLAPS(CONTROL SURFACES)
• FINS
• EFFICIENCY
• AIR TO AIR MISSILES
• AIR TO SURFACE MISSILES
• SURFACE TO AIR MISSILES
• GUIDED BOMBS
• GRAPHS

Subject Categories:

• Guided Missiles
• Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE