Part I. Following an accident to a Mosquito fitted experimentally by the Royal Aircraft Establishment with a g-restriction device involving heavy mass-overbalance of an elevator tab, an investigation has been made into the ...

Pitching-moment derivatives have been measured, using a free-oscillation technique, for a series of thin tapered wings with both streamwise and raked tips. Wings of three aspect ratios (A.R. = 2.74, 2.00 and 1.25) were ...

The requirements for simulating in a Wind tunnel flutter conditions appropriate to high-speed flight are discussed, and an assessment is made of the desirable features of a wind tunnel suitable for flutter testing at ...