Design of a large-scale model for wind tunnel test of a multiadaptive flap concept

Author:

SICIM DEMIRCI Mürüvvet Sinem,PECORA RosarioORCID,KAYA Metin Orhan

Funder

Clean Sky Joint Technology Initiative

TÜBİTAK

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference36 articles.

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2. Effects of wing flexibility on aerodynamic performance of an aircraft model;Guo;Chin J Aeronaut,2021

3. Design and manufacturing of aerospace composite structures, state-of-the-art assessment;Harris;J Aircr,2002

4. Brissenden RF, Heath AR, Conner DW. Assessment of variable camber for application to transport aircraft. Washington, D.C.: NASA; 1980. Report No.: CR-158930.

5. Design, modeling, and control of morphing aircraft: a review;Chu;Chin J Aeronaut,2022

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