Prediction of transonic shock-induced separation for 40° lambda wings

41st Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2003, Pages

  McParlin, Stephen C ^a   Adamczak, David W ^b  

^a QINETIQ   (United Kingdom)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84894755017     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. st AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, 6-9 Jan 2003.
2. Parker N. T. and Ayres J. C., "Mach and Reynolds number effects on a 40-lambda planform half-wing model (M2389), phase 1 tests. " DERA/AS/ASD/CR97076/1, March 1997.
3. st Congress of the International Congress of Aeronautical Sciences, Melbourne, Australia, 14-18 September 1998.
4. 60 Users Manual, " Air Force Research Lab/VAAC, July 2000.
5. Godunuv S. K., "A Difference Scheme for Numerical Computation of Discontinuous Solutions of Hydrodynamic Equations, " Sbornik Mathematics, Vol. 47, pp. 271-306, 1959.
6. Samareh J., "GridTool: "A Surface Modelling and Grid Generation Tool, Proceedings of the Workshop on Surface Modelling, Grid Generation, and Related issues in CFD solutions, NASA CP-3291 May 1995.