Exact(16)
However, Southwest had replaced some fuselage panels subject to the testing.
Aircraft wing and fuselage panels are often built in multibay configurations.
Crenellation is a promising technique to effectively improve the fatigue life of fuselage panels.
Stiffened fuselage panels with laminated constructions play an increasing role in aircraft design.
Full-scale tests were conducted on fuselage panels cut from retired aircraft.
The work presented investigates a methodology for the implementation of value-driven design (VDD) with application to the optimisation of aircraft fuselage panels.
Similar(44)
Applied to an aircraft fuselage panel, the method estimates cost and mass of different production alternatives.
To predict the residual strength of a curved fuselage panel with discrete source damage using the R-curve method, G-curves of the energy release rate of the damaged fuselage panel need to be established.
This study applies the crack growth resistance curve (R-curve) method to predict the residual strength of a composite fuselage panel with discrete source damage.
Tapering a thin fuselage panel layup to a thicker layup at the countersunk hole proved highly effective in achieving satisfactory joint strength and energy absorption.
The residual strength of the damaged fuselage panel was determined by comparing the energy release rates with the "allowable-like" R-curve.
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