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1. (76)	Original version of the author's contribution as presented on CD, POS. : PDF Traction drive of an electric vehicle using an ultracapacitor Huták, P. ; Vorel, P. This paper describes an usage of ultra-capacitors in the system electric drive + traction accumulator. The purpose of the ultra-capacitor in this application is to increa [...] Detailed record - Similar records
2. (77)	Original version of the author's contribution as presented on CD, FLU. : PDF Preliminary interferometry measurements of flow field around a fluttering NACA0015 profile Vlček, V. ; Kozánek, J. The paper presents experimental results of the optical measurements of flow field around a fluttering NACA0015 profile elastically supported with two degrees of freedom i [...] Detailed record - Similar records
3. (78)	Original version of the author's contribution as presented on CD, . : PDF Dynamic and stability properties of an aeroelastic model Horáček, J. ; Veselý, J. Frequency modal and damping characteristics of an aeroelastic model designed for experiments in the wind tunnel are studied. Based on the experimental modal analysis the [...] Detailed record - Similar records
4. (79)	Original version of the author's contribution as presented on book, page 99. : PDF LANDING SHOCK AEROELASTIC RESPONSE ANALYSIS OF UTILITY AIRCRAFT Čečrdle, J. The paper deals with the aircraft landing shock aeroelastic response analysis. The analysis was performed as a part of the aircraft certification in order to fulfill the [...] Detailed record - Similar records
5. (80)	Original version of the author's contribution as presented on CD, , page 13. : PDF Updating of aircraft dynamic model according results of ground vibration test Čečrdle, J. Detailed record - Similar records
6. (80)	Original version of the author's contribution as presented on CD, . : PDF SIMULATION OF FLUTTER USING CFD-FEM COUPLED MODEL Losík, V. So far the static as well as dynamic aeroelastic tasks have been commonly solved by using linear models of fluid flow (p-k method, DLM) implemented e.g. in system MSC.Nas [...] Detailed record - Similar records
7. (86)	Original version of the author's contribution as presented on CD, . : PDF OPTIMIZATION OF THE COMMUTER AIRCRAFT WING STIFFNESS CHARACTERISTICS CONSIDERING REQUIREMENT OF AEROELASTIC STABILITY AT THE CERTIFICATION SPEED Čečrdle, J. The submitted paper deals with aeroelastic optimization. It gives a summary of theory with special regard to the aeroelasticity. Main part describes optimization of the a [...] Detailed record - Similar records
8. (100)	Original version of the author's contribution as presented on CD, DYN. : PDF Assessment of aileron tab installation influence to ultra-light aircraft flutter characteristics Čečrdle, J. Submitted paper deals with the aileron flutter of the ultra-light aircraft. It gives an assessment of influence of the additional installation of the tab regarding the ai [...] Detailed record - Similar records

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