Abstract:
This thesis concerns the crashworthiness of
helicopters onto water and presents a
comparison between test and simulation for the impact of a typical helicopter sub floor
section onto both hard and water surfaces. The
experimental campaign was extended to
incorporate a fully instrumented WG30 helicopter drop test onto water, which allowed a
comprehensive assessment of the predictive capabilities of the non-linear code LS-
DYNA3D to be
performed.
Validation data was
supplied from specific drop tests, which permitted a complete
frarne-by-frame analysis to be performed and compared both quantitively and
qualitatively with the numerical results. The conclusions from this work enabled a
assessment of the
validity of the component and full-scale simulations with respect to
one another, together with the design changes that could potentially improve the level of
crashworthiness
currently offered with the current design.
Modelling the compressive behaviour of a fluid using a Lagrangian approach is difficult,
due to the inherent mesh
problems associated with large definitions. Sensitivity
studies were
performed, which led to the development of a tuned water model that was
capable of recreating the impact of various rigid shapes onto water. Alternative
techniques to water modelling are also presented in a attempt to minimise the stability
problems that arise between fluid and structure boundary, where the definite elements
attempt to form a splash. To complete this review of the capabilities of the code, a
assessment with
respect to capturing joint failure was also performed, through
comparison with joint coupon tests.
As no
methodology concerning the simulation of fluid-structure interaction problems
exists within the literature, this thesis addresses this issue by discussing the
contributions made to the SAFESA approach (SAFE Structural Analysis), in identifying
potential sources of error that are relevant when performing these types of analysis. A
discussion of the sources of idealisation, procedural and formulation errors will be
performed, along with techniques and recommended practices that have been developed
to minimise their affects. The
methodology has been extensively tested to be a robust
and reliable
approach that will greatly assist engineers working in this field.
The culmination of this research is the
application of the validated simulation tools in
developing a potential solution for improving the water crashworthiness response. The
concept of maximising skin defection through the purposeful collapse of the
interconnecting frames is presented. This would allow the skin to form a continuous
curve, as opposed to several inter frame defections. The numerical results verify that
this
hypothesis could be of benefit in reducing the magnitudes of the accelerations and
raises the
question of whether next generation designs should concentrate on developing
energy absorbing characteristics for each individual cell, or whether a coupled, multiple
cell
configuration is more preferable.