dc.contributor.author | Mukherjee, Bijoy Krishna | |
dc.date.accessioned | 2018-02-26T09:39:20Z | |
dc.date.available | 2018-02-26T09:39:20Z | |
dc.date.issued | 2017-12-01 | |
dc.identifier.govdoc | NB15939 | |
dc.identifier.uri | http://www.idr.iitkgp.ac.in/xmlui/handle/123456789/8864 | |
dc.language.iso | en | en |
dc.publisher | IIT, Kharagpur | en |
dc.subject | Optimal Trim Strategy | en |
dc.subject | Asymmetric Dynamics | en |
dc.subject | Fighter Aircraft Dynamics | en |
dc.subject | Aircraft Flight Mechanics | en |
dc.subject | Civil Aircraft | en |
dc.title | Nonlinear Dynamics and Control of a Laterally Mass Varying Fighter Aircraft Operating at High Angles-of-Attack | en |
dc.type | Thesis | en |