Results 221 to 230 of about 231,983 (247)
This paper reviews recent advances in hybrid deep learning for intelligent fault diagnosis of rotating machinery, focusing on GAN‐ and CNN‐based architectures and their specialized variants. Hybrid GAN‐CNN methods are categorized into three groups: (1) optimized original GANs with CNN variants, (2) improved GAN architectures integrated with CNNs, and ...
Temesgen Tadesse Feisa +7 more
wiley +1 more source
Addressing platelet insecurity - A national call to action. [PDF]
Gehrie EA +14 more
europepmc +1 more source
ABSTRACT We present a hybrid interpretable Physics‐Informed Neural Network Long‐Short Term Memory (Hybrid PINN LSTM) framework for predicting the seismic response of rocking blocks. Existing analytical models rely on uncertain idealizations, while purely data‐driven and machine‐learning approaches lack physical consistency and interpretability.
Shirley Shen +1 more
wiley +1 more source
Tribological and Corrosion Properties of Coatings of Ultradisperse TiB<sub>2</sub>-TiAl Electrodes with Nanosized Additives Deposited on Ti-Gr2 by Non-Contact Electrospark Deposition. [PDF]
Kostadinov G +9 more
europepmc +1 more source
Experimental demonstration of tractor millimeter wave beam propulsion. [PDF]
Takahashi M +4 more
europepmc +1 more source
Hypersonic turbulent quantities in support of Morkovin's hypothesis. [PDF]
Segall BA +6 more
europepmc +1 more source
Coexistence of detonation with deflagration in rotating detonation engines
Rotating detonation engines of high thermal efficiency and specific impulse have been studied a lot. However, rotating detonation waves lead to uneven flow field, local high temperature and high pressure, tending to damage the combustor.
Yuhui Wang
exaly +2 more sources
Critical condition of inner cylinder radius for sustaining rotating detonation waves in rotating detonation engine thruster [PDF]
We describe the critical condition necessary for the inner cylinder radius of a rotating detonation engine (RDE) used for in-space rocket propulsion to sustain adequate thruster performance. Using gaseous C2H4 and O2 as the propellant, we measured thrust
Ikkoh Funaki +2 more
exaly +2 more sources
The feasibility of mode control in rotating detonation engine
The feasibility of mode control in rotating detonation engine is investigated through regulating the global equivalence ratio during the test under different air mass flow rates, chamber lengths, and blockage ratios at the exit, including the mode ...
Xiao Liu, Changsheng Zhou
exaly +2 more sources

