Conditions of Result Approach while Using Airfoil's Measurement Data for Calculation of Wing's Lifting Force

Abstract:

• Periodical: Solid State Phenomena (Volume 113)
• Pages: 489-494
• DOI: https://doi.org/10.4028/www.scientific.net/SSP.113.489
• Online since: June 2006
• Authors: E. Pakalnis, E. Lasauskas, J. Stankūnas
• Keywords: Airfoil, Lifting Force, Wing

References

[1] G. S. Campbell: A Finite-Step Method for the Calculation of Span Loadings of Unusual Plan Forms (NACA RM L50L13, 1951).

[2] A. J. Blackwell: A Finite-Step Method for Calculation of Theoretical Load Distributions for Arbitrary Lifting-Surface Arrangements at Subsonic Speeds (NASA TN D-5335, July 1969).

[3] J. P. Barnes: Semi-Empirical Vortex Step Method for the lift and induced drag loading of 2D and 3D Wings (Society of Automotive Engineers, SAE Paper 975559, Oct. 1997), pp.1-18.

DOI: 10.4271/975559

[4] R. Mukherjee, A. Gopalarathnam and S. W. Kim: An Iterative decambering Approach for PostStall prediction of Wing Characteristics Using Known Section Data (AIAA 2003-1097), pp.1-11.

DOI: 10.2514/6.2003-1097

[5] K. Jacob: Computation of the Flow around Wings with Rear Separation (Journal of Aircraft 21, 1984), pp.97-98.

DOI: 10.2514/3.48230

[6] E. Lasauskas, E. Pakalnis and J. Stankūnas: System of non Linera Equations for Calculation of Wing Lift Force (Aviacija, No 6, Vilnius. Technika, 2002), pp.50-54 (in Lithuanian).

[7] E. Pakalnis, E. Lasauskas and J. Stankūnas: Method to Evaluate Nonlinear Effect in Calculation of a Finite Span Wing (Scientific proceedings of Riga Technical University, Vol. 7, Transport and Engineering. Aviation Transport, 2003), pp.223-228.

[8] E. Pakalnis, E. Lasauskas and J. Stankūnas: Convergence of Lift Force Calculation of a Tapered Wing Using Non-Linear Section Data (Mechanika No 1 (51), 2005), pp.61-65.