Sökning: L773:1270 9638 > Investigation of li...
Fältnamn | Indikatorer | Metadata |
---|---|---|
000 | 01971naa a2200337 4500 | |
001 | oai:DiVA.org:kth-45556 | |
003 | SwePub | |
008 | 111031s2004 | |||||||||||000 ||eng| | |
024 | 7 | a https://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-455562 URI |
024 | 7 | a https://doi.org/10.1016/j.ast.2003.08.0062 DOI |
040 | a (SwePub)kth | |
041 | a engb eng | |
042 | 9 SwePub | |
072 | 7 | a ref2 swepub-contenttype |
072 | 7 | a art2 swepub-publicationtype |
100 | 1 | a Berggren, Danielu KTH,Flygteknik4 aut0 (Swepub:kth)u17q4qxt |
245 | 1 0 | a Investigation of limit cycle oscillations for a wing section with nonlinear stiffness |
264 | 1 | b Elsevier BV,c 2004 |
338 | a print2 rdacarrier | |
500 | a QC 20111031 | |
520 | a A wind tunnel experiment is designed with the objective to obtain well-behaved limit cycle oscillations for a wing section with two degrees of freedom, translation and rotation, in two-dimensional flow. This is accomplished using a setup of linear springs so that the resulting moment is a nonlinear function of the rotation angle. The experimental setup is designed so that the amplitudes of the limit cycle oscillations are sufficiently low to motivate the use of linear aerodynamics in the analysis. The experimental results are compared to analyses for two different configurations, and the agreement is fairly good. | |
650 | 7 | a TEKNIK OCH TEKNOLOGIERx Maskinteknikx Rymd- och flygteknik0 (SwePub)203022 hsv//swe |
650 | 7 | a ENGINEERING AND TECHNOLOGYx Mechanical Engineeringx Aerospace Engineering0 (SwePub)203022 hsv//eng |
653 | a nonlinear | |
653 | a aeroelasticity | |
653 | a structural dynamics | |
653 | a unsteady aerodynamics | |
710 | 2 | a KTHb Flygteknik4 org |
773 | 0 | t Aerospace Science and Technologyd : Elsevier BVg 8:1, s. 27-34q 8:1<27-34x 1270-9638x 1626-3219 |
856 | 4 8 | u https://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-45556 |
856 | 4 8 | u https://doi.org/10.1016/j.ast.2003.08.006 |
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