Aerodynamic diagnostics and design based on boundary vorticity dynamics

17th Applied Aerodynamics Conference

Volumn , Issue , 1999, Pages 33-46

  Wu, J Z ^a   Roach, R L ^a   Lo, C F ^a   Zhu, F L ^a   Dowgwillo, R M ^b   Jiang, L B ^c   Tramel, R W ^d  

^a UNIVERSITY OF TENNESSEE SPACE INSTITUTE   (United States)

^b BOEING COMPANY   (United States)

^c Chinese Aeronautical Establishment   (United States)

^d Micro Craft Inc   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; HYPERSONIC FLOW; MACH NUMBER; TRANSONIC FLOW; VORTEX FLOW; VORTICITY;

BOUNDARY VORTICITY FLUXES; CONVENTIONAL APPROACH; INVERSE DESIGNS; LEADING-EDGE VORTICES; LOW-MACH-NUMBER FLOW; MOMENT FORMULA; NEW APPROACHES; VORTICITY DYNAMICS;

BODIES OF REVOLUTION;

EID: 84964240933     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

1. Wu, J.Z. and Wu, J.M. 1989. Vortical sources of aerodynamic force and moment. SAE TP 892346.
2. Wu, J.Z. and Wu, J.M. 1993. Interactions between a solid surface and a viscous compressible flow field. J. Fluid Mech. 254, 183-211.
3. Wu, J.Z. and Wu, J.M. 1996. Vorticity dynamics on boundaries. Adv. Appl. Mech. 32, 119-275.
4. Wu, J.Z. and Wu, J.M. 1998. Boundary vorticity dynamics since Lighthill’s 1963 article. Theoret. Comput. Fluid Dyn. 10, 459-474.
5. Lighthill, M.J. 1963. Introduction: Boundary layer theory. In Laminar Boundary Layers, ed. by L. Rosenhead, Cambridge Univ. Press. 46-113.
6. Wu, J.M., Ondrusek, B., and Wu, J.Z. 1996. Exact force diagnostics of vehicles based on wake-plane data. AIAA Paper 96-0559.
7. Wu, J.Z. and Wu, J.M. 1987. A new theoretical basis for optimal aerodynamic design by wind-tunnelcomputer integration. Proc. 2nd Intern. Conf. Inverse Design Concepts and Optimization in Engineering Sciences, Oct. 26-28, 1987, Pennsylvania.
8. Yamamoto, K. and Inoue, O. 1995. Application of genetic algorithm to aerodynamic shape optimization. AIAA 95-1650.
9. Buning, P.G, et al. 1998. OVERFLOW user’s manual, version 1.8, NASA Langey Research Center, Hampton VA.
10. Roach, R.L. and Jekins, J.E. 1995. Improvements to the numerical simulation of pitching delta wings. AIAA Paper 95-0761.
11. Gätzke, T., Dowgwillo, R., and Ikeda, Y. 1998. The design of an aerodynamic fairing using viscous computational fluid dynamics. AIAA Paper 982787.
12. Wu, J.Z., Yin, X.Y., Tramel, R.W., and Zhu, F.L. 1998. A theory of fully three-dimensional flow separation along generic separation line. Submitted to AIAA 30th Fluid Dynamics Conference, 1999