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TsAGI Science Journal

ISSN Druckformat: 1948-2590
ISSN Online: 1948-2604

TsAGI Science Journal

DOI: 10.1615/TsAGISciJ.v40.i3.90
pages 393-399

DESIGN OF A MULTIPURPOSE AEROELASTIC MODULAR MODEL

V. A. Malyutin
Central Aerohydrodynamic Institute (TsAGI) 1, Zhukovsky str., Zhukovsky, 140180, Moscow region, Russia

ABSTRAKT

A multipurpose aeroelastic modular model of the lift surface of a high-aspect-ratio aircraft is considered. A beam structural scheme is used for the simulation of model stiffness characteristics. An algorithm for the determination of model design parameters based on the requirement of stiffness characteristic similarity is proposed. Design results for the elastically scaled model of a high-aspect-ratio wing are presented.

REFERENZEN

  1. Bisplinghoff, R. L., Ashley, H., and Halfman, R. L., Aero elasticity.

  2. Azarov, Yu. A., Zichenkov, M. Ch., Ishmuratov, F. Z., and Chedrick, V. V., Design methods of dynamically-scaled models of airplane units.

  3. Amiryants, G. A., Anosova, L. V., Efimenko, S. V., Ishmuratov, F. Z., Kolushov, N. M., Malyutin, V. A., and Mullov, Yu. M., Multi-purpose aeroelastical modular model of an aircraft.

  4. Amiryants, G. A., Universal aerodynamic model and the method of its manufacturing.

  5. Amiryants, G. A., Latsoev, K. F, Malyutin, V. A., Mullov, Yu. M., and Nayko, Yu. A., Station for determination of stiffness characteristics of structures and their aerodynamic/aeroelastic models.

  6. Schittkowski, K., More Test Examples for Nonlinear Programming Codes.


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