Development of wing deflection assessment methods through experimental ground tests and finite element analysis

Author:

Gharibi Ali,Ovesy Hamid Reza,Khaki Reza

Publisher

Elsevier BV

Subject

Mechanical Engineering,Building and Construction,Civil and Structural Engineering

Reference27 articles.

1. V.M. DeAngelis., R. Fodale, Electro-optical flight deflection measurement system, in: Proceedings of the 18th Annual Symposium on Society of Flight Test Engineers, SFTE Technical Paper, 22, 1987, pp. 1–14.

2. W.A. Lokos, Predicted and Measured In-Flight Wing Deflections of a Forward-Swept-Wing Aircraft, NASATM-4245, 1990

3. V.M. DeAngelis, In-Flight Deflection Measurement of the HiMATAeroelastically Tailored Wing, AIAA-81-2450, 1981

4. K.L. Bonnema, W.A. Lokos, AFTI/F-111 mission adaptive wing flight test instrumentation overview, Paper No. 89-0084, in: Proceedings of the 35th International Instrumentation Symposium, Instrument Society of America, North Carolina, 1989.

5. Videogrammetric model deformation measurement technique;Burner;J. Aircr.,2001

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