Aerodynamic indicial functions and their use in aeroelastic formulation of lifting surfaces

41st Structures, Structural Dynamics, and Materials Conference and Exhibit

Volumn , Issue , 2000, Pages

  Marzocca, Picrgiovanni ^a   Librescu, Liviu ^a   Silva, Walter A ^b  

^a State University   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTICITY; FREQUENCY DOMAIN ANALYSIS; LIME; STRUCTURAL DYNAMICS;

AERODYNAMIC DERIVATIVES; AERODYNAMIC MOMENT; CLOSED FORM SOLUTIONS; FURTHER DEVELOPMENT; GRAPHICAL REPRESENTATIONS; INDICIAL FUNCTIONS; SUBCRITICAL RESPONSE; TIME AND FREQUENCY DOMAINS;

LIFT;

EID: 85086492137     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-0     Document Type: Conference Paper

References (10)

1. Barmby, J.G., Cunningham, HJ. & Garrick, I.E., "Study of Effects of Sweep on the Flutter of Cantilever Wings. " NACA Report No. 1014, 1951.
2. Bisplinghoff, R.L., Ashley, H. & Halfman R.L., "Aeroelasticitv. " Dover, 1955.
3. Edwards, J.W., Ashley, H. & Breakwell, J.V., "Unsteady Aerodynamic Modeling for Arbitrary Motions. " AIAA Journal, Vol. 17, pp. 365-374, 1979, presented as AIAA Paper 77-451 at the AIAA Dynamics Specialist Conference, San Diego, California, 1977.
4. Flax, A.H., "Aeroelasticity and Flutter, in High Speed Problems of Aircraft and Experimental Methods. " in Vol. VIII "Hieh Speed Aerodynamics and Jet Propulsion" Eds. Donovan, H.F. and Lawrence, H.R., Princeton University Press, 1961, pp.161-417.
5. Karpouzian, G. & Librescu, L., "Comprehensive Model of Anisotropic Composite Aircraft Wings Suitable for Aeroelastic Analyses. " Journal of Aircraft, Vol. 31, No. 3, May-June, pp. 703-712, 1994.
6. Karpouzian, G. & Librescu, L., "Non-Classical Effects on Divergence and Flutter of Anisotropic Swept Aircraft Wings, " AIAA Journal, Vol. 34, No. 4, April, pp.786-794, 1996.
7. Librescu, L. & Thangjitham, S., "Analytical Studies on Static Aeroelastic Behavior of Forward Swept Composite Wing Structures. " Journal of Aircraft, Vol. 28, No. 2, pp. 151-157, 1991.
8. Scanlan, R.H., "Aeroelastic Problems of Civil Engineering Structures. " in "A Modern Course in Aeroelasticitv. " Dowell, E.H. editor, Kluwer Academic Publishers, Third Revised and Enlarged Edition, 1996.
9. nd Ed., Wiley, NY, 1986.
10. Yates, C., "Calculation of Flutter Characteristics for Finite-Span Swept or Unswept Wings at Subsonic and Supersonic Speeds by a Modified Strip Analysis. " NACA RM No. L57L10, March 1958.