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Keywords: Transient flow analysis
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Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2019) 91 (1): 10–19.
Published: 13 November 2018
... 2017 09 08 2017 The section hinge moment is defined as follows: (1) h = 1 2 ρ ( Ω r ) 2 c f 2 C h If integrated spanwise, the result is: Structural integrity Static bench test Trailing-edge flap Transient flow analysis Vertical pulling test...
