Simulation of limit cycle oscillation of fighter aircraft at moderate angle of attack
Simulation of limit cycle oscillation of fighter aircraft at moderate angle of attack
| dc.contributor.author | Prananta, B.B. | en_US |
| dc.contributor.author | Kok, J.C. | en_US |
| dc.contributor.author | Spekreijse, S.P. | en_US |
| dc.contributor.author | Hounjet, M.H.L. | en_US |
| dc.contributor.author | Meijer, J.J. | en_US |
| dc.date.accessioned | 2013-10-23T08:18:41Z | |
| dc.date.available | 2013-10-23T08:18:41Z | |
| dc.date.issued | 2003 | en_US |
| dc.identifier.other | NLR-TP-2003-526 | en_US |
| dc.identifier.uri | http://hdl.handle.net/10921/644 | |
| dc.language.iso | en | en_US |
| dc.publisher | National Aerospace Laboratory NLR | en_US |
| dc.relation.ispartofseries | NLR Technical Publication;2003-526 | en_US |
| dc.subject.other | Aeroelasticity / unsteady flow | en_US |
| dc.subject.other | Structural dynamics / vibration | en_US |
| dc.title | Simulation of limit cycle oscillation of fighter aircraft at moderate angle of attack | en_US |
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