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Design-Optimierung
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NASA Integrated Model-Centric Architecture (NIMA)
Reliability Estimation for Mission Extension NASA Approach/Recommendations
Challenges in Adjoint-Based Aerodynamic Design for Unsteady Flows
Aeroelastic Optimization of Generalized Tube and Wing Aircraft Concepts Using HCDstruct Version 2.0
Aeroelastic Tailoring Study of N+2 Low-Boom Supersonic Commercial Transport Aircraft
NDARC NASA Design and Analysis of Rotorcraft - Input, Appendix 10
Aeroelastic Tailoring Study of N+2 Low Boom Supersonic Commerical Transport Aircraft
Rapid Analysis & Manufacturing Propulsion Technology (RAMPT)
Comprehensive Digital Transformation NASA Langley Research Center
Basis Function Approximation of Transonic Aerodynamic Influence Coefficient Matrix
Basis Function Approximation of Transonic Aerodynamic Influence Coefficient Matrix