Please use this identifier to cite or link to this item: https://doi.org/10.4271/940028
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dc.titleNonlinear analysis of flight dynamics at large angles of attack and sideslip
dc.contributor.authorLeng, G.
dc.date.accessioned2014-06-19T09:10:20Z
dc.date.available2014-06-19T09:10:20Z
dc.date.issued1994
dc.identifier.citationLeng, G. (1994). Nonlinear analysis of flight dynamics at large angles of attack and sideslip. SAE Technical Papers. ScholarBank@NUS Repository. <a href="https://doi.org/10.4271/940028" target="_blank">https://doi.org/10.4271/940028</a>
dc.identifier.urihttp://scholarbank.nus.edu.sg/handle/10635/75050
dc.description.abstractResults from nonlinear dynamical systems theory are used in understanding fighter aircraft flight dynamics at large angles of attack and sideslip. Instabilities encountered at large angles of attack and sideslip like pitch-up, nose-slice, wing-rock are readily examined within the context of bifurcation theory. An example of nonlinear analysis using a reduced order model and a combined symbolic/numeric computational approach is discussed. It will be shown that dynamical systems theory provides useful guidelines for flight simulation and testing at large angles of attack and sideslip.
dc.description.urihttp://libproxy1.nus.edu.sg/login?url=http://dx.doi.org/10.4271/940028
dc.sourceScopus
dc.typeConference Paper
dc.contributor.departmentMECHANICAL & PRODUCTION ENGINEERING
dc.description.doi10.4271/940028
dc.description.sourcetitleSAE Technical Papers
dc.identifier.isiutNOT_IN_WOS
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