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title: AIAA Journal of Aircraft
Boundary Layer Ingestion Benefit of the D8 Transport Aircraft
Boundary Layer Ingestion Benefit of the D8 Transport Aircraft
Results from the Sixth AIAA Computational Fluid Dynamics Drag Prediction Workshop: Case 1 Code Verification are presented. This test
...AIAA Manuscript Review Process
AIAA Manuscript Review Process
AIAA Manuscript Review Process
AIAA Manuscript Review Process
AIAA Manuscript Review Process
Summary of the Fourth AIAA Computational Fluid Dynamics Drag Prediction Workshop
Summary of the Fourth AIAA Computational Fluid Dynamics Drag Prediction Workshop
DLR Results from the Fourth AIAA Computational Fluid Dynamics Drag Prediction Workshop
DLR Results from the Fourth AIAA Computational Fluid Dynamics Drag Prediction Workshop
Flexible Aircraft Simulation Validation with Flight Test Data
The challenges of modeling flexible aircraft include appropriate fidelity capturing and validation with experimental data. In fact, the
...Vertical Drop Test of Composite Fuselage Section of a Regional Aircraft
In this paper, a vertical drop test of a full composite fuselage section of a regional aircraft has been presented. This test was
...Noise Characteristics of Aircraft High Lift Systems
High-Fidelity Modeling of Multirotor Aerodynamic Interactions for Aircraft Design
Electric aircraft technology has enabled the use of multiple rotors in novel concepts for urban air mobility. However, multirotor
...Application of the FUN3D Solver to the 4th AIAA Drag Prediction Workshop
Application of the FUN3D Solver to the 4th AIAA Drag Prediction Workshop
Geometric Programming for Aircraft Design Optimization
Formulating conceptual-stage aircraft design problems as geometric programs, which are a specific type of convex optimization problem
...Coupled Aerostructural Level Set Topology Optimization of Aircraft Wing Boxes
In this paper, the wing box of an aircraft is optimized using a level set topology optimization method and considering aerostructural
...Three-Way Spectral Decompositions of High-Performance Military Aircraft Noise
Experimental Investigation of Fluid–Structure Interaction Phenomena During Aircraft Ditching