±3-Sigma based design optimization of 3D Finocyl grain
0–1 integer programming model for procedural separation of aircraft by ground holding in ATFM
2.2. Structural model and aeroelastic equations of motion in generalized modal form
2.3. Aerodynamic model and generalized unsteady air forces
2.4.1. Two-dimensional SDOF typical blade section analysis
2.4.2. Three-dimensional SDOF flutter analysis
2.4. Combustors with and without dome cowls
2.4. Single-blade-degree-of-freedom flutter analysis in modal form
2.5.1. Formulation of the flutter problem
2.5.2. Structural coupling features of the flexible blade-disc-shroud assembly
2.5. Multiple-blade-degrees-of-freedom flutter analysis in modal form
2.5. Vortex controlled and hybrid diffusers