Wind tunnel tests of a long range artillery shell concept

AIAA Atmospheric Flight Mechanics Conference and Exhibit

Volumn , Issue , 2002, Pages

  Dupuis, A ^a   Berner, C ^b  

^a DEFENCE RESEARCH AND DEVELOPMENT CANADA VALCARTIER   (Canada)

^b FRENCH GERMAN RESEARCH INSTITUTE OF SAINT LOUIS   (France)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; FINS (HEAT EXCHANGE); ORDNANCE; PROJECTILES;

ANGLES OF ATTACK; ARTILLERY PROJECTILE; LIFTING SURFACES; LONG-RANGE ARTILLERY; NORMAL FORCES; ROLL MOMENT; SEMI-EMPIRICAL; WIND TUNNEL TESTS;

WIND TUNNELS;

EID: 85087191087     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-4416     Document Type: Conference Paper

References (5)

1. Fleck, V., Berner, C., Increase of Range for an Artillery Projectile by Using the Lift Force, Proceedings 16th International Ballistics Symposium, San Francisco, CA, USA, 23-27 September 1996, ISL Report PU 355/96
2. "Commissioning Report of the DREV 2ft. Indraft Wind Tunnel", Dilworth, Secord, Meagher and Associates Ltd., Report No. 695/912, March 1977
3. Projectile Design Analysis System (PRODAS), P2000 V 2.2.17, Arrow Tech Associates Inc., 2000
4. Moore, F. G., McInville, R., M. and Hymer, T., The 1995 Version of the NSWC Aeroprediction Code: Part I - Summary of New Theoretical Methodology, Naval Surface Weapons Center, NSWCCDD/TR-94/379, February 1995
5. Burns, K. A., Deters, K. J., Stoy, S. L., Vukelich, S. R. and Blake, W. B, Missile Datcom Users Manual - Revision 6/93, WL-TR-93-3043, June 1993.