The elastic deformation of modern projectiles with large slenderness ratio cannot be ignored
with the increasing of flight speed and maneuverability. Unsteady Reynolds-averaged …

Obvious aeroelastic deformation occurs in spinning projectiles with large slenderness ratio,
which seriously affects flight stability and maneuverability. This paper investigates the …

The structural rigidity of a spinning missile with large slenderness ratio is usually small, and
the structural deformation and rate should not be ignored. Furthermore, rotational motion …

There are aerodynamic and inertial couplings in rigid-body motion and structural vibration of
a flexible spinning missile in flight, and when slenderness ratio is larger, the couplings are …

The general equations of motion of a flexible spinning missile under thrust in the powered
flight phase are established and the stability of the motion of the missile is analyzed. The …

Since projectiles with large slenderness ratio are prone to elastic deformation, the effect of
structural deformation is necessary to be taken into consideration for dynamic modeling. In …

To deliver heavier payloads to longer ranges as the main objective of tactical missiles,
higher slenderness and thrust-to-weight ratios are sought. This leads to the emergence of …

A numerical methodology based on the coupling of computational fluid dynamics (CFD) and
computational structural dynamics is established to obtain the trimming characteristics of …

In order to improve the cost-effectiveness ratio, the next-generation vehicle needs to meet
the requirements of reuse, while adopting a lighter structural weight, so it is necessary to …