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FVM J 23
Wing Shape Multidisciplinary Design Optimization
Dept. of Aerospace Engineering
Static Aeroelasticity Using High Fidelity Aerodynamics in a Staggered Coupled and ROM Scheme
Vortex Dynamics Study of the Canard Deflection Angles' Influence on The
Conceptual Multidisciplinary Aircraft Design Using Aero-Structural Adjoint-Based Methods Andrea Viti
Vehicledesignevaluation
A Study of Nonlinear Flight Control System Designs Lijun Tian Iowa State University
PARASOL FIGHTERS the FVM J 23 & J 24/J 24B
Shape and Sizing Optimization of Aircraft Structures with Aeroelastic and Induced Drag Requirements
Manifestation of the Finite Vortex—Lift, Thrust and Drag 249
B.E. Aeronautical Engineering
Performance Analysis of a Coaxial Helicopter in Hover and Forward Flight
EVALUATION of ADVANCED LIFT CONCEPTS Nm ~' O
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