Results 121 to 130 of about 238,845 (361)
Report on the Examination of I Stage Compressor Blades [PDF]
, 1989 The damages suffered by I stage compressor blades of three aeroengines have been studied at the request of Indian Air ...
Raghuram, AC +2 more
core
Advanced Engineering Materials, EarlyView.Equal channel angular pressing of commercial pure copper under low strain amplitude (≈0.48) induces concurrent continuous and localized discontinuous dynamic recrystallization, forming a duplex structure influenced by strain heterogeneity and recovery. Moderate hardening after 4–12 passes results from progressive high‐angle grain boundary formation via
Paula Cibely Alves Flausino +6 more
wiley +1 more source
Discussion: “Skewed Boundary-Layer Flow Near the End Walls of a Compressor Cascade” (Moore, Jr., R. W., and Richardson, D. L., 1957, Trans. ASME, 79, pp. 1789–1797) [PDF]
, 1957 Richard E. Kronauer
openalex +3 more sources
Advanced Engineering Materials, EarlyView.This study compares the mechanical properties of Inconel 718 with two newly developed compositionally complex alloys (CCAs). Inco‐like‐H alloy demonstrates significantly improved wear resistance, surface finish, and hardness, notably at high temperatures. This CCA requires no heat treatment and is well suited for additive manufacturing. Its performance
Laurent Peltier +3 more
wiley +1 more source
LubricantsIn aerospace applications, engine parts, especially those around the rotor blade tips, are coated with an abradable seal, a specific material layer. Its design produces a tighter seal without harming the blades by allowing it to wear down or “abrade ...
Anitha Kumari Azmeera +2 more
doaj +1 more source
Design of a miniature hydrogen fueled gas turbine engine [PDF]
The design, development, and delivery of a miniature hydrogen-fueled gas turbine engine are discussed. The engine was to be sized to approximate a scaled-down lift engine such as the teledyne CAE model 376.
Burnett, M. +6 more
core +1 more source
Discussion: “A New Method of Calculation of Repeat Factors for Turbines and Compressors” (Kaye, Joseph, and Wadleigh, K. R., 1951, ASME J. Appl. Mech., 18, pp. 387–392) [PDF]
, 1952 D. J. Bloomberg
openalex +1 more source
Advanced Engineering Materials, EarlyView.A machine learning‐driven framework is introduced to optimize 3D‐printable microneedles for enhanced tissue anchoring and reduced insertion damage. The optimized design achieves a 6.0‐fold improvement in pull‐out‐to‐penetration energy ratio over conventional shapes.
Jegyeong Ryu +5 more
wiley +1 more source
Study on thermal analysis simulation and test of propellant refueling process for optical module
Xibei Gongye Daxue XuebaoPropellant refueling is important for long-term operation of the optical module in orbit. However, its thermal environment is harsher than on previous missions. Therefore, thermal control of the entire process is required.
LU Wei +4 more
doaj +1 more source