Researchers developed a projection-based reduced-order model integrating isogeometric analysis and energy-conserving hyper-reduction to rapidly simulate parameterized liquid sloshing in aerospace ...
Mathematical modelling reveals that birds flap while landing because unpowered stops require excessive approach speeds and space.
Researchers used response surface methodology to determine optimal drilling parameters for surface roughness and material removal rate in AA7075-T6 aluminium ...
A finite element analysis reveals that steel-aluminium bimetallic beams perform best at high temperatures, while invar-aluminium pairs excel in cryogenic ...
Simulations demonstrate that an extended multi-model switching and tuning control strategy achieves accurate fault diagnosis and reduces attitude deviations for ...
Aerospace researchers have designed a distributed two-layer control protocol that enables hypersonic vehicle swarms to achieve optimal output consensus while ...
A computational investigation reveals how angle of attack, Mach number, and rarefaction govern shock wave detachment, recirculation, and particle flux ...
Computational fluid dynamics simulations demonstrate that pairing a ramp-chevron injector with an internal air jet significantly alters supersonic hydrogen mixing ...
Researchers modeled the roll-out deployment of a bistable laminated composite tubular boom, calculating its driving force and predicting deployment velocity, ...
A new two-fluid turbulence model reproduces NASA benchmark data for a Mach 1.63 supersonic jet more accurately than the conventional ...
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