Aeroelasticity of two-dimensional lifting surfaces via indicial function approach

Aeronautical Journal

Volumn 106, Issue 1057, 2002, Pages 147-153

  Marzocca, P ^a   Librescu, L ^a   Chiocchia, G ^b  

^a Virginia Polytechnic Institute and State University   (United States)

^b POLITECNICO DI TORINO   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL SYSTEMS; DEGREES OF FREEDOM (MECHANICS); DYNAMIC LOADS; FEEDBACK CONTROL; FREQUENCY DOMAIN ANALYSIS; FUNCTIONS; LAPLACE TRANSFORMS; PROBLEM SOLVING; SURFACE TREATMENT;

AEROELASTIC EQUATIONS; CLOSED-LOOP AEROELASTIC RESPONSE; PLUNGING;

AERODYNAMICS;

EID: 0041794053     PISSN: 00019240     EISSN: None     Source Type: Trade Journal    
DOI: None     Document Type: Article

References (11)

1. BISPLINGHOFF, R.L., ASHLEY, H. and HALFMAN, R.L. Aeroelasticity, Dover Publications, New York, 1996.
2. MARZOCCA, P., LIBRESCU, L. and CHIOCCHIA, G. Aeroelastic response of a 2D lifting surfaces to gust and arbitrary explosive loading signatures, Int J Impact Eng, 2001, 25, (1), pp 41-65.
3. LIBRESCU, L. and NOSIER, A Response of laminated composite flat panels to sonic-boom and explosive blast loading, AIAA J, 1990, 28, (2), pp 345-352.
4. KARPEL, L. Design for active flutter suppression and gust alleviation using state-space aeroelastic modelling. J Aircr. 1982, 19, (3), pp 221-227.
5. EDWARDS, J.W., ASHLEY, H. and BREAKWELL, J.V. Unsteady aerodynamic modelling for arbitrary motions. AIAA J, 1979, 17, (4), pp 365-374. presented as AIAA-77-451 at the AIAA Dynamics Specialist Conference, San Diego, California, 1977.
6. EDWARDS, J.W., ASHLEY, H. and BREAKWELL, J.V. Unsteady aerodynamic modelling for arbitrary motions. AIAA J, 1979, 17, (4), pp 365-374. presented as AIAA-77-451 at the AIAA Dynamics Specialist Conference, San Diego, California, 1977.
7. FUNG, Y.C. An introduction to the Theory of Aeroelasticiiy, John Wiley, New York, 1955.
8. MAZEESKY, B. Charts of airplane acceleration ratio for gusts of arbitrary shape. NACA TN 2036, February 1950, p 18.
9. HOUBOLT, J.C. and KORDES, E E. Structural response to discrete and continuous gusts of an airplane having wing bending flexibility and a correlation of calculated and flight results, NACA Rpt 1181, 1954, p 22, Supersedes NACA TN 3006.
10. SEARS, WR, and SPARKS, B.O. On the reaction of an elastic wing to vertical gusts, J Aeronaut Sci, 1941, 9, pp 64-67.
11. LEISHMAN, J.G. Validation of approximate indicial aerodynamic functions for two-dimensional subsonic flow. J Aircr, 1988, 25, (10), pp 914-922.