A CFD based study of UCAV 1303 model

Collection of Technical Papers - AIAA Applied Aerodynamics Conference

Volumn 1, Issue , 2005, Pages 189-197

  Zhang, F ^a   Khalid, M ^a   Ball, N ^a  

^a NATIONAL RESEARCH COUNCIL CANADA   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AEROSPACE ENGINEERING; COMPUTATIONAL FLUID DYNAMICS; COMPUTATIONAL METHODS; MATHEMATICAL MODELS; WINGS;

AERODYNAMIC PERFORMANCE; EDGE DESIGNS; SWEPT WINGS; UCAV 1303 MODEL;

AEROSPACE VEHICLES;

EID: 28844490241     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-4615     Document Type: Conference Paper

References (6)

1. http://flash.icemcfd.com/index.html
2. NPARC User's Guide- NASA LeRC/AEDC Alliance, Version 3.0, Sep. 1996. Washington.
3. Cooper, G. K. and Sirbaugh, J. R., "Parc Code: Theory and Usage", AEDC-TR-89-15, Sverdrup Technolgy Inc.
4. F. Zhang, M. Khalid, H. Xu and N. Ball, "Numerical Prediction of the Reflection Plate Boundary Layer Effects on Half Model in Wind Tunnel", AIAA-2000-2376, Jun. 2000, Denver, USA.
5. F. Zhang, M. Khalid, J. Syms and N. Ball, Numerical Investigation of the Aerodynamic Performance of the Aurora CP-140 Aircraft, 48th Annual Conference, Canadian Aeronautics and Space Institute, April 29 - May 2, 2001, Toronto, Canada.
6. A. R. G. Mundell, Test conditions for 1303 UCAV (M2445) in 5m Tunnel, Technical Report, July 2002, UK.