Accession Number:

AD0901791

Title:

Experimental Aerodynamic Characteristics of a Fluidic-Controlled, Antitank Missile with Wraparound Fins at Mach Numbers from 0.2 to 3.0. Volume III. Tabulation of Pressure Data.

Descriptive Note:

Technical rept.,

Corporate Author:

ARMY MISSILE RESEARCH DEVELOPMENT AND ENGINEERING LAB REDSTONE ARSENAL AL AER OBALLISTICS DIRECTORATE

Personal Author(s):

• Street, Troy A.
• Killough, Thomas L.

Report Date:

1971-12-03

Pagination or Media Count:

582.0

Abstract:

This report of pressure data tables contains pages numbered 807 through 1385. The Page Index of the various configurations tested covers Volumes 1, 2 and 3.

Descriptors:

• *FLUIDICS
• *GUIDED MISSILE MODELS
• *FLIGHT CONTROL SYSTEMS
• PRESSURE
• FINS
• CONTROL JETS
• INTERACTIONS
• SUBSONIC CHARACTERISTICS
• TRANSONIC CHARACTERISTICS
• SUPERSONIC CHARACTERISTICS
• ROLL
• YAW
• PITCH(MOTION)
• ANTITANK AMMUNITION
• FIN STABILIZED AMMUNITION
• WIND TUNNEL MODELS
• ANGLE OF ATTACK
• FORCE(MECHANICS)
• EXPERIMENTAL DATA
• TABLES(DATA)

Subject Categories:

• Fluidics and Fluerics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE