The symmetric flutter and response characteristics of a class of tailless .sailplanes-:are investigated combining rigid--body dynamics with elastic modes of deformation. The methods used are based on the normal mode approach ...
A computer program is developed to determine the buckling stress
and deflections of symmetric corrugated core sandwich panels. In
the program freedom for lateral deflections at core to face-plate
junction is allowed ...
Effects of various wing-body interaction design
parameter variations on the structural behaviour of
a small RPV have been investigated using the finite
element method on an adhoc basis rather than a classical
analytic ...