Vortex-oscillation model of airfoil side-edge noise

AIAA Journal

Volumn 35, Issue 3, 1997, Pages 441-449

  Sen, R ^a,b  

^a BOEING COMPANY   (United States)

^b Mail Stop 67 LF   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROFOILS; NOISE; OSCILLATIONS; VORTEX FLOW;

EID: 0031006890     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.149     Document Type: Article

References (6)

1. Miller, W. R., "Flap Noise Characteristics Measured by Pressure CrossCorrelation Techniques ," Ph.D. Thesis, Dept. of Mechanical, Aerospace, and Nuclear Engineering, Univ. of California, Los Angeles, CA, 1980.
2. Crighton, D. G., "Airframe Noise," Aeroacoustics of Flight Vehicles: Theory and Practice, edited by H. H. Hubbard, Vol. I, NASA RP 1258, 1991.
3. Hardin, J. C, "Noise Radiation from the Side Edges of Flaps," AlAA Journal, Vol. 18, No. 5, 1980, pp. 549-552.
4. Saffman, P. G., Vortex Dynamics, Cambridge Univ. Press, New York, 1992, Chap. 7.
5. Bender, C. M., and Orszag, S. A., Advanced Mathematical Methods for Scientists and Engineers, McGraw-Hill, New York, 1978, Chap. 4.
6. Hénon, M., "Numerical Exploration of Hamiltonian Systems," Chaotic Behavior of Deterministic Systems, edited by G. looss, R. H. G. Helleman, and R. Stora, USMG/NATO ASI Session 36 (Les Houches, France), NorthHolland, Amsterdam, 1983.