Limit loading and wing frequency tests of the composite VUK-T sailplanes
Апстракт
A test program aimed for the limit loading and frequency characteristics testing of the wings of the first all-composite sailplane, VUK-T, designed in Yugoslavia was presented. The verification test implied combined frequency-static-frequency testing. The wings were mounted on a special ground-fixed rigid mount in inverted position, at an incidence that simulated the actual angle of attack at which maximum wing loading was achieved in flight. The ground testing procedure proved to be reliable and efficient in determining the capability of the wings to withstand the limit loading without consequences for the structure.
Кључне речи:
Static and frequency wing tests / Limit wing loading / Composite sailplaneИзвор:
Proceedings of the Mini Conference on Vehicle System Dynamics, Identification and Anomalies, 2000, 429-436Scopus: 2-s2.0-0346368586
Колекције
Институција/група
Mašinski fakultetTY - CONF AU - Dragović, T. AU - Kostić, Ivan PY - 2000 UR - https://machinery.mas.bg.ac.rs/handle/123456789/184 AB - A test program aimed for the limit loading and frequency characteristics testing of the wings of the first all-composite sailplane, VUK-T, designed in Yugoslavia was presented. The verification test implied combined frequency-static-frequency testing. The wings were mounted on a special ground-fixed rigid mount in inverted position, at an incidence that simulated the actual angle of attack at which maximum wing loading was achieved in flight. The ground testing procedure proved to be reliable and efficient in determining the capability of the wings to withstand the limit loading without consequences for the structure. C3 - Proceedings of the Mini Conference on Vehicle System Dynamics, Identification and Anomalies T1 - Limit loading and wing frequency tests of the composite VUK-T sailplanes EP - 436 SP - 429 UR - https://hdl.handle.net/21.15107/rcub_machinery_184 ER -
@conference{ author = "Dragović, T. and Kostić, Ivan", year = "2000", abstract = "A test program aimed for the limit loading and frequency characteristics testing of the wings of the first all-composite sailplane, VUK-T, designed in Yugoslavia was presented. The verification test implied combined frequency-static-frequency testing. The wings were mounted on a special ground-fixed rigid mount in inverted position, at an incidence that simulated the actual angle of attack at which maximum wing loading was achieved in flight. The ground testing procedure proved to be reliable and efficient in determining the capability of the wings to withstand the limit loading without consequences for the structure.", journal = "Proceedings of the Mini Conference on Vehicle System Dynamics, Identification and Anomalies", title = "Limit loading and wing frequency tests of the composite VUK-T sailplanes", pages = "436-429", url = "https://hdl.handle.net/21.15107/rcub_machinery_184" }
Dragović, T.,& Kostić, I.. (2000). Limit loading and wing frequency tests of the composite VUK-T sailplanes. in Proceedings of the Mini Conference on Vehicle System Dynamics, Identification and Anomalies, 429-436. https://hdl.handle.net/21.15107/rcub_machinery_184
Dragović T, Kostić I. Limit loading and wing frequency tests of the composite VUK-T sailplanes. in Proceedings of the Mini Conference on Vehicle System Dynamics, Identification and Anomalies. 2000;:429-436. https://hdl.handle.net/21.15107/rcub_machinery_184 .
Dragović, T., Kostić, Ivan, "Limit loading and wing frequency tests of the composite VUK-T sailplanes" in Proceedings of the Mini Conference on Vehicle System Dynamics, Identification and Anomalies (2000):429-436, https://hdl.handle.net/21.15107/rcub_machinery_184 .