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):
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