Tez Dosyaları 4
Development of a high-fidelity transient aerothermal model for a helicopter turboshaft engine for inlet distortion and engine deterioration simulations
Aerodynamic parameter estimation of a supersonic missile with rapid speed variation by using kalman filtering
Kill analysis tool for missiles equipped with proximity fuzes
Stochastic and deterministic analysis of nonlinear of nonlinear missile engagement scenarios using 5-dof 6-dof and adjoint model