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1.	Original version of the author's contribution in proceedings, page 234, section DYN.: PDF AIRCRAFT WING FLUTTER ASSESSMENT CONSIDERING DAMAGE TOLERANCE - BASED FAILURE STATES Čečrdle, J. ; Raška, J. This paper deals with aircraft wing flutter analysis considering the failure states, originated by the application of the damage - tolerance design philosophy on the wing [...] Detailed record - Similar records
2.	Original version of the author's contribution as presented on CD, , page 11. : PDF Whirl flutter optimisation-based solution of twin turboprop aircraft using full-span model Čečrdle, J. 21 Detailed record - Similar records
3.	Original version of the author's contribution as presented on CD, id 025, section DYN.: PDF MECHANICAL CONCEPT OF WHIRL FLUTTER AEROELASTIC DEMONSTRATOR Čečrdle, J. ; Vích, O. This paper deals with the design of the whirl flutter aeroelastic demonstrator. It gives a theoretical background of the whirl flutter phenomenon. The main part is focuse [...] Detailed record - Similar records
4.	Original version of the author's contribution as presented on CD, paper (No. 015).: PDF Aeroelastic certification of light sport aircraft according "LTF" regulation Čečrdle, J. ; Hlavatý, V. Submitted paper deals with the aeroelastic certification of a light sport aircraft according the German regulation standard "LTF-UL". The procedure is simple, fast and lo [...] Detailed record - Similar records
5.	Original version of the author's contribution as presented on CD, paper No. 19.: PDF INFLUENCE OF PROPELLER BLADE FORCE SPANWISE DISTRIBUTION ON WHIRL FLUTTER CHARACTERISTICS Čečrdle, J. This paper is focused on the influence of the propeller blade lift spanwise distribution on whirl flutter stability. It gives the theoretical background of the whirl flut [...] Detailed record - Similar records
6.	Original version of the author's contribution as presented on CD, 114. : PDF NASPRO 3.0 – software tool for transformation and vizualization of aircraft structure modal analysis results Čečrdle, J. ; Gallovič, D. The submitted paper presents a new software tool named NASPRO 3.0 aimed for transformation and visualization of the aircraft modal characteristics. The mode shapes are vi [...] Detailed record - Similar records
7.	Original version of the author's contribution as presented on CD, , page 112. : PDF DETERMINATION OF AIRCRAFT STRUCTURE WHIRL FLUTTER STABILITY BOUNDARIES BY MEANS OF OPTIMIZATION BASED SOLUTION Čečrdle, J. The submitted paper deals with the aircraft structure whirl flutter analysis. It gives a summary of the regulations requirements, the theoretical background and the aircr [...] Detailed record - Similar records
8.	Original version of the author's contribution as presented on CD, DYN. : PDF AEROELASTIC SENSITIVITY ANALYSIS OF AIRLINER WING Čečrdle, J. ; Vích, O. This paper describes the airliner wing flutter sensitivity analysis. The sensitivity coefficients define the influence of the structural parameters changes to the structu [...] Detailed record - Similar records
9.	Original version of the author's contribution as presented on CD, , paper No. 119. : PDF Whirl flutter analysis of the commuter aircraft aeroelastic model wing -- engine component Čečrdle, J. The submitted paper deals with whirl flutter of turboprop aircraft. It gives a summary of the airworthiness regulations requirements and the theoretical background concer [...] Detailed record - Similar records
10.	Original version of the author's contribution as presented on CD, . : PDF X-dia demonstrator aeroelastic test – design, analysis and model wind tunnel support tuning Čečrdle, J. Submitted paper deals with preparation of the X-DIA aeroelastic demonstrator component wind tunnel tests. Paper is focused to design, analysis and manufacturing of new co [...] Detailed record - Similar records

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