Open Access Articles

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Performance assessment of low-by-pass turbofan engines for low-boom civil supersonic aircraft
Studies in hydrogen micromix combustor technologies for aircraft applications
Ten years of aero-servo-elastic tests at large POLIMI’s wind tunnel for active flutter control and loads alleviation
Aeroelastic design and optimization of strut-braced high aspect ratio wings
New insights on limit cycle oscillations due to control surface freeplay
Wind tunnel flutter tests of a strut-braced high aspect ratio wing
Tiltrotor whirl-flutter stability analysis using the maximum Lyapunov characteristic exponent estimated from time series
Predicting noise spectrum of a small drone rotor in a confined environment: a lattice Boltzmann Vles analysis
On the influence of airframe flexibility on rotorcraft pilot couplings
Experimental investigation of the noise emitted by two different propellers ingesting a planar boundary layer
Aeroacustics computation based on harmonic balance solution
Leonardo I4N research program – design of novel acoustic liners for aero engine nacelles