A continuation method for the calculation of airfoil flutter boundaries

35th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1997, Pages

  Beran, Philip S ^a   Morton, Scott A ^b  

^a Air Force Institute of Technology   (United States)

^b WRIGHT PATTERSON AIR FORCE BASE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AEROSPACE ENGINEERING; AIRFOILS; FLUTTER (AERODYNAMICS); STRUCTURAL DYNAMICS;

AUTOMATED PROCEDURES; CONTINUATION ALGORITHM; CONTINUATION METHOD; FREESTREAM MACH NUMBER; STRUCTURAL COUPLING; STRUCTURAL DAMPING; STRUCTURAL PARAMETER; TIME-DOMAIN TECHNIQUE;

TIME DOMAIN ANALYSIS;

EID: 84983156564     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)

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2. Farr, J.L., Traci, R.M. & Albano, E.D., Computer Programs for Calculating Small Disturbance Transonic Flows about Oscillating Airfoils, AFFDL-TR-74-135, November, 1974.
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9. Morton, S.A. & Beran, P.S., Hopf-Bifurcation Analysis of Airfoil Flutter at Transonic Speeds, 34th Aerospace Sciences Meeting, Reno, NV, January, 1996. AIAA Paper 96-0060.
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11. Seydel, R., From Equilibrium to Chaos: Practical Bifurcation and Stability Analysis, Elsevier Science Publishing Co., Inc., 1988.
12. Smith, M.D., Schuster, D., Huttsell, L., & Buxton, B.J., Development of an Euler/Navier-Stokes Aeroelastic Method for Three-Dimensional Vehicles with Multiple Flexible Structures. Proceedings of the 37th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Salt Lake, UT, April, 1996. AIAA Paper 96-1513.
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