Application of Wagner functions in symmetrical airfoil design

Journal of Aircraft

Volumn 34, Issue 2, 1997, Pages 259-260

  Onur, N ^a  

^a GAZI UNIVERSITY   (Turkey)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER AIDED DESIGN; DESCRIBING FUNCTIONS; FOURIER TRANSFORMS; POLYNOMIALS;

THIN AIRFOIL THEORY; WAGNER FUNCTION SERIES;

AIRFOILS;

EID: 0031095461     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.7573     Document Type: Article

References (7)

1. Braembussche, R. V. D., "Special Course on Inverse Methods for Airfoil Design for Aeronautical and Turbomachinery Applications," AGARD-R-780, Nov. 1990.
2. McGroskey, W. J., and Peckham, D. H., Computational Methods for Aerodynamic Design (Inverse) and Optimization, CP-463, AGARD, March 1990.
3. Periaux, J., "Optimum Design Methods for Aerodynamics," AGARD-R-803, Nov. 1994.
4. Ramamoorthy, P., Dwarakanath, G. S., and Narayana, C. L., "Wagner Functions," National Aeronautical Lab., TN 16, Bangalore 17, India, 1969.
5. Clancy, L. J., Aerodynamics, Pitman Publishing Co., 1975.
6. Abbot, I. H., and Von Doenhoff, A. E., Theory of Wing Sections, McGraw-Hill, New York, 1959.
7. Seilig, M. S., Maughmert, M. D., and Somers, D. M., "Natural-Laminar-Flow Airflow for Generating-Aviation Applications," Journal of Aircraft, Vol. 23, No. 4, 1995, pp. 710-715.