Organizational Unit:
Aerospace Systems Design Laboratory (ASDL)
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A methodology to support relevant comparisons of Earth-Mars communication architectures
A nonparametric-based approach on the propagation of imprecise probabilities due to small datasets
Aerothermodynamic cycle design and optimization method for aircraft engines
A parametric and physics-based approach to structural weight estimation of the hybrid wing body aircraft
Development and validation of 3-D cloud fields using data fusion and machine learning techniques
Compressor conceptual design optimization
A combined global and local methodology for launch vehicle trajectory design-space exploration and optimization
A methodology for conducting design trades related to advanced in-space assembly
A methodology for capturing the impacts of bleed flow extraction on compressor performance and operability in engine conceptual design
Numerical simulation of ice accretion on 3-D rotor blades