Aeroelastic scaling for rotary-wing aircraft with applications

Journal of Fluids and Structures

Volumn 19, Issue 5, 2004, Pages 635-650

  Friedmann, P P ^a  

^a UNIVERSITY OF MICHIGAN   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

MATHEMATICAL MODELS; VIBRATION CONTROL; VIBRATION MEASUREMENT; WINGS;

AEROELASTIC SCALING; ROTARY-WING AIRCRAFTS;

AERODYNAMICS;

AERODYNAMICS; AEROELASTICITY; FLUID-STRUCTURE INTERACTION; ROTOR; WING;

EID: 3042675647     PISSN: 08899746     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.jfluidstructs.2004.03.003     Document Type: Article

References (21)

1. Baker, W.E., Westine, P.S., Dodge, F.T., 1991. Similarity Methods in Engineering Dynamics: Theory and Practice of Scale Modeling, Revised Edition. Elsevier, Amsterdam.
2. Barenblatt G.I. Scaling, Self-similarity, and Intermediate Asymptotics 1996 Cambridge University Press Cambridge
3. Bisplinghoff R.L. Ashley H. Halfman R.L. Aeroelasticity 1955 Addison-Wesley Publishing Co. Cambridge, MA, USA
4. Chopra I. Status and application of smart structures technology to rotorcraft systems Journal of the American Helicopter Society 45 4 2000 228-252
5. de Terlizzi, M., Friedmann, P.P., 1999. Active control of bvi induced vibrations using a refined aerodynamic model and experimental correlation. In: Proceedings of the 55th Annual Forum of the American Helicopter Society, Montreal, Canada, pp. 599-615.
6. Friedmann, P.P., 1998. Rotary-wing aeroelastic scaling and its application to adaptive materials based actuation. In: Proceedings of the 39th AIAA/ASME/AHS/ASC Structures, Structural Dynamics, and Materials Conference and AIAA/ASME Adaptive Structures Forum No. AIAA Paper 98-2698, Long Beach, CA, USA.
7. Friedmann, P.P., Hodges, D.A., 1993. Rotary-wing aeroelasticity with application to vtol vehicles. In: Noor, A.K., Venneri, S.L. (Eds.), Flight Vehicles, Materials, Structures, and Dynamics-Assessment and Future Directions, Vol. 5. ASME, New York, pp. 299-391 (Chapter 6).
8. Friedmann P.P. Presente E. Active control of flutter in compressible flow and its aeroelastic scaling Journal of Guidance, Control and Dynamics 24 1 2001 167-177
9. Friedmann P.P. Guillot D. Presente E. Adaptive control of aeroelastic instabilities in transonic flow and its scaling Journal of Guidance, Control and Dynamics 20 6 1997 1190-1199
10. Fulton, M.V., Ormiston, R.A., 1998. Small-scale rotor experiments with on-blade elevons to reduce blade vibratory loads in forward flight. In: Proceedings of the 54th Annual Forum of the American Helicopter Society, Washington, DC, USA, pp. 433-451.
11. Hunt, G.K., 1973. Similarity requirements for aeroelastic models of helicopter rotors. CP 1245, Aeronautical Research Council.
12. Lazarus K.B. Crawley E.F. Lin C.Y. Multivariable active lifting surface control using strain actuation: Analytical and experimental results Journal of Aircraft 34 3 1997 313-321
13. Lin C.Y. Crawley E.F. Heeg J. Open- and closed-loop results of a strain-actuated active aeroelastic wing Journal of Aircraft 33 5 1996 987-994
14. Mueller, T.J. (Ed.), 2001. Fixed and flapping wing aerodynamics for micro air vehicle applications. In: Progress in Astronautics and Aeronautics, Vol. 195. AIAA, New York.
15. Myrtle T.F. Friedmann P.P. Application of a new compressible time domain aerodynamic model to vibration reduction in helicopters using an actively controlled flap Journal of the American Helicopter Society 46 1 2001 32-43
16. Regier, A.A., 1963. The use of scaled dynamic models in several aerospace vehicle studies. In: Proceedings of ASME Colloquium on the Use of Models and Scaling in Simulation of Shock and Vibration. Philadelphia, PA, ASME, New York, pp. 34-50.
17. Singleton J.D. Yeager W.T. Important scaling parameters for testing model-scale helicopter rotors Journal of Aircraft 37 3 2000 396-402
18. Straub F.K. Johnston R.A. Head R.E. Design and development of a dynamically scaled model ah-64 main rotor Vertica-the International Journal of Rotorcraft and Powered Lift Aircraft 9 2 1985 165-180
19. Theodorsen, T., 1935. General theory of aerodynamic instability and the mechanism of flutter. Technical Report 496, NACA August.
20. Theodorsen, T., Garrick, I.E., 1942. Nonstationary flow about a wing-aileron-tab combination including aerodynamic balance. Technical Report 736, NACA.
21. Venkatesan, C., Friedmann, P.P., 1984. Aeroelastic effects in multi-rotor vehicles with applications to a hybrid heavy lift system, part i: Formulation of equations of motion, NASA CR 3822, NASA AMES Research Center, CA, USA.