Optimal rectangular end plates

Journal of Aircraft

Volumn 33, Issue 3, 1996, Pages 623-625

  Standingford, D W F ^a   Tuck, E O ^a  

^a UNIVERSITY OF ADELAIDE   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; LIFT COEFFICIENT; RECTANGULAR END PLATES; SKIN FRICTION; TWO DIMENSIONAL FLOW;

DRAG; FRICTION; INTEGRAL EQUATIONS; LIFT; OPTIMIZATION; PLATES (STRUCTURAL COMPONENTS); VORTEX FLOW; WINGS;

AIRCRAFT PARTS AND EQUIPMENT;

EID: 0030149382     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/3.46991     Document Type: Article

References (6)

1. Ashley, H., and Landahl, L., Aerodynamics of Wings and Bodies, Addison-Wesley, New York, 1965, pp. 124-148.
2. Tuck, E. O., "Lifting Surfaces with Endplates," Proceedings of the 11th Australasian Fluid Mechanics Conference, edited by M. R. Davis and G. J. Walker, Univ. of Tasmania, Australia, 1992, pp. 219-222.
3. Standingford, D. W. F., Lazauskas, L. V., and Tuck, E. O., "On the Numerics of the Lifting Surface Equation," Applied Mathematics Dept., Univ. of Adelaide, Adelaide, Australia, 1995.
4. Tuck, E. O., "Some Accurate Solutions of the Lifting Surface Equation," Journal of the Australian Mathematical Society (Series B), Vol. 35(2), Oct. 1993, pp. 127-144.
5. Lan, C. E., "A Quasi-Vortex-Lattice Method in Thin Wing Theory," Journal of Aircraft, Vol. 11, No. 9, 1974, pp. 518-527.
6. Turrill, D., "Wings and Free Speed," Open Wheel Magazine, May 1992, p. 63.