Determining Rotor Blade Multi-Mode Vibration Components †.
- Published in:
- Applied Sciences (2076-3417), 2025, v. 15, n. 9, p. 4883, doi. 10.3390/app15094883
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- Article
Works matching DE "COMPRESSOR blades"
Results: 490
1
2
A deep neural network with attention mechanism for flow prediction of compressor blade.
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- Scientific Reports, 2025, v. 15, n. 1, p. 1, doi. 10.1038/s41598-025-99688-0
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- Publication type:
- Article
3
Hovering rotor computations using an aeroelastic blade model.
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- Aeronautical Journal, 2012, v. 116, n. 1180, p. 621, doi. 10.1017/S0001924000007107
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- Publication type:
- Article
4
Trailing-edge flap flow control for dynamic stall.
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- Aeronautical Journal, 2011, v. 115, n. 1170, p. 493, doi. 10.1017/S0001924000006138
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- Publication type:
- Article
5
A framework for optimising aspects of rotor blades.
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- Aeronautical Journal, 2011, v. 115, n. 1165, p. 147, doi. 10.1017/S0001924000005558
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- Article
6
Analysis of turbine performance degradation effects due to geometry variations between actual components and design Intent.
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- Aeronautical Journal, 2010, v. 114, n. 1159, p. 569, doi. 10.1017/S0001924000004048
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- Article
7
Validation study for prediction of iced aerofoil aerodynamics.
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- Aeronautical Journal, 2010, v. 114, n. 1152, p. 103, doi. 10.1017/S0001924000003572
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- Article
8
Numerical and experimental investigation of tip leakage flow and heat transfer using idealised rotor-tip models at transonic conditions.
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- Aeronautical Journal, 2009, v. 113, n. 1141, p. 165, doi. 10.1017/S0001924000011453
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- Article
9
Survivability of helicopter with individual blade primary control failure.
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- Aeronautical Journal, 2007, v. 111, n. 1124, p. 645, doi. 10.1017/S0001924000004826
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- Article
10
Measuring the effect of helicopter rotors on GPS reception.
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- Aeronautical Journal, 2007, v. 111, n. 1123, p. 561, doi. 10.1017/S0001924000001834
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- Publication type:
- Article
11
A wind-tunnel based study of helicopter tail rotor blade vortex interaction.
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- Aeronautical Journal, 2004, v. 108, n. 1083, p. 237, doi. 10.1017/S0001924000005091
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- Publication type:
- Article
12
Analysis of anisotropic prismatic sections.
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- Aeronautical Journal, 2004, v. 108, n. 1082, p. 197, doi. 10.1017/S0001924000000105
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- Publication type:
- Article
13
Control laws for an active tunable vibration absorber designed for rotor blade damping augmentation.
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- Aeronautical Journal, 2004, v. 108, n. 1079, p. 35, doi. 10.1017/S0001924000004978
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- Article
14
Optimizing hot forging parameters for gas turbine blade formation: a comprehensive study.
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- International Journal of Advanced Manufacturing Technology, 2024, v. 133, n. 3/4, p. 1563, doi. 10.1007/s00170-024-13825-z
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- Publication type:
- Article
15
Enhancing machinability of Ti6Al4V by ultrashort-pulse laser-induced modification assisted grinding.
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- International Journal of Advanced Manufacturing Technology, 2023, v. 125, n. 9/10, p. 4601, doi. 10.1007/s00170-023-11073-1
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- Publication type:
- Article
16
Analysis and design optimization of double-sided deep cold rolling process of a Ti-6Al-4V blade.
- Published in:
- International Journal of Advanced Manufacturing Technology, 2020, v. 108, n. 7/8, p. 2103, doi. 10.1007/s00170-020-05481-w
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- Article
17
Tool path planning for five-axis flank milling of free-form surfaces.
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- International Journal of Advanced Manufacturing Technology, 2020, v. 108, n. 1/2, p. 73, doi. 10.1007/s00170-020-05283-0
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- Publication type:
- Article
18
Optimal milling modes identification of a jet-engine blade using time-domain technique.
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- International Journal of Advanced Manufacturing Technology, 2020, v. 107, n. 5/6, p. 1983, doi. 10.1007/s00170-020-05129-9
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- Article
19
Design and implementation of hybrid force/position control for robot automation grinding aviation blade based on fuzzy PID.
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- International Journal of Advanced Manufacturing Technology, 2020, v. 107, n. 3/4, p. 1741, doi. 10.1007/s00170-020-05061-y
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- Publication type:
- Article
20
Synthesis and characterization of non-equiatomic Ti0.3AlMoSi0.3W0.1 high-entropy alloy fabricated via spark plasma sintering.
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- International Journal of Advanced Manufacturing Technology, 2020, v. 107, n. 1/2, p. 679, doi. 10.1007/s00170-020-05062-x
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- Article
21
Force modeling for polishing aero-engine blades with abrasive cloth wheels.
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- International Journal of Advanced Manufacturing Technology, 2020, v. 106, n. 11/12, p. 5255, doi. 10.1007/s00170-020-05016-3
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- Article
22
Accurate model construction of deformed aero-engine blades for remanufacturing.
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- International Journal of Advanced Manufacturing Technology, 2020, v. 106, n. 7/8, p. 3239, doi. 10.1007/s00170-019-04688-w
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- Article
23
Localization method for precision forged blade edge considering multiple constraints.
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- International Journal of Advanced Manufacturing Technology, 2019, v. 104, n. 9-12, p. 4641, doi. 10.1007/s00170-019-04233-9
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- Article
24
Conventional rotational molding process and aerodynamic characteristics of an axial-flow hollow blades rotor.
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- International Journal of Advanced Manufacturing Technology, 2019, v. 104, n. 1-4, p. 1183, doi. 10.1007/s00170-019-03962-1
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- Article
25
5-axis grinding path generation for free-form surface based on plane instantaneous grinding engagements.
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- International Journal of Advanced Manufacturing Technology, 2019, v. 103, n. 5-8, p. 1861, doi. 10.1007/s00170-019-03664-8
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- Article
26
Trajectory planning of abrasive belt grinding for aero-engine blade profile.
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- International Journal of Advanced Manufacturing Technology, 2019, v. 102, n. 1-4, p. 605, doi. 10.1007/s00170-018-3187-z
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- Article
27
A force-measuring-based approach for feed rate optimization considering the stochasticity of machining allowance.
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- International Journal of Advanced Manufacturing Technology, 2018, v. 97, n. 5-8, p. 2545, doi. 10.1007/s00170-018-2127-2
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- Article
28
Optimization of machining strip width using effective cutting shape of flat-end cutter for five-axis free-form surface machining.
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- International Journal of Advanced Manufacturing Technology, 2018, v. 94, n. 5-8, p. 2623, doi. 10.1007/s00170-017-0953-2
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- Article
29
An adaptive repair surface modeling approach for worn blades.
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- International Journal of Advanced Manufacturing Technology, 2018, v. 94, n. 1-4, p. 523, doi. 10.1007/s00170-017-0859-z
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- Article
30
Shape optimization of regenerative flow compressor with aero-foil type blades using response surface methodology coupled with CFD.
- Published in:
- Structural & Multidisciplinary Optimization, 2021, v. 64, n. 4, p. 2653, doi. 10.1007/s00158-021-03020-z
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- Article
31
Surrogate based optimization of helicopter rotor blades for vibration reduction in forward flight.
- Published in:
- Structural & Multidisciplinary Optimization, 2008, v. 35, n. 4, p. 341, doi. 10.1007/s00158-007-0137-z
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- Article
32
Numerical evaluation of the aerodynamic influence of the helicopter composite blade trailing edge tabs.
- Published in:
- Archive of Applied Mechanics, 2007, v. 77, n. 12, p. 893, doi. 10.1007/s00419-007-0133-1
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- Article
33
Spherical Fixed Abrasive Head Lapping of Titanium Alloy.
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- Strength of Materials, 2024, v. 56, n. 6, p. 1251, doi. 10.1007/s11223-025-00735-y
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- Article
34
Stability Limits of GTE Axial Compressor Blade Rings for Subsonic Bending-Torsion Cascade Flutter on Stalling and Nonstalling Flow.
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- Strength of Materials, 2023, v. 55, n. 2, p. 277, doi. 10.1007/s11223-023-00522-7
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- Article
35
Effect of Complex Magnetic-Abrasive and Chemical-Thermal Treatment on the Fatigue Resistance of VT8 Alloy Compressor Blades.
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- Strength of Materials, 2020, v. 52, n. 6, p. 947, doi. 10.1007/s11223-021-00248-4
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- Article
36
Correction to: Effect of Porosity Parameters on the Strength of Gas Turbine Compressor Blades Made of Titanium Alloys.
- Published in:
- 2020
- By:
- Publication type:
- Correction Notice
37
Effect of Porosity Parameters on the Strength of Gas Turbine Compressor Blades Made of Titanium Alloys.
- Published in:
- Strength of Materials, 2019, v. 51, n. 6, p. 887, doi. 10.1007/s11223-020-00139-0
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- Article
38
Rapid method of Predicting the Subsonic Flutter Stability of AGTE Axial-Flow Compressor Blade Cascades. Part 2. Mathematical Implementation of Method and its Potentional Application.
- Published in:
- Strength of Materials, 2019, v. 51, n. 5, p. 689, doi. 10.1007/s11223-019-00117-1
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- Article
39
Rapid Method of Predicting the Subsonic Flutter Stability of AGTE Axial-Flow Compressor Blade Cascades. Part 1. Physical Backgrounds of the Method.
- Published in:
- Strength of Materials, 2019, v. 51, n. 2, p. 175, doi. 10.1007/s11223-019-00063-y
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- Publication type:
- Article
40
Gas Dynamic Action of Annular Blowing on the Aerodynamic Factors of the Resonance Vibration Excitation of Rotor Blades in a Compressor Stage.
- Published in:
- Strength of Materials, 2018, v. 50, n. 2, p. 317, doi. 10.1007/s11223-018-9974-9
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- Article
41
On Modeling of the Blading Sections of Compressors with Dynamic Compression in Compression of Real Gases.
- Published in:
- Chemical & Petroleum Engineering, 2016, v. 51, n. 11/12, p. 825, doi. 10.1007/s10556-016-0129-1
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- Publication type:
- Article
42
Contact-Free Slit Rotor Seals with a Controllable Shape of the Throttle Slit.
- Published in:
- Chemical & Petroleum Engineering, 2003, v. 39, n. 5/6, p. 281, doi. 10.1023/A:1025671217463
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- Article
43
Procedure for Analyzing Rotor Equipment with Flow Modulation.
- Published in:
- Chemical & Petroleum Engineering, 2003, v. 39, n. 5/6, p. 305, doi. 10.1023/A:1025631603351
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- Publication type:
- Article
44
Numerical analysis of air supply parameters and non‐uniform characteristics in a cover‐plate pre‐swirl system with the adjustable flow path.
- Published in:
- International Journal of Energy Research, 2021, v. 45, n. 6, p. 8763, doi. 10.1002/er.6412
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- Article
45
Performance comparison of different combined heat and compressed air energy storage systems integrated with organic Rankine cycle.
- Published in:
- International Journal of Energy Research, 2019, v. 43, n. 14, p. 8410, doi. 10.1002/er.4839
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- Article
46
Axial-flow compressor analysis under distorted phenomena at transonic flow conditions.
- Published in:
- Cogent Engineering, 2018, v. 5, n. 1, p. 1, doi. 10.1080/23311916.2018.1526458
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- Publication type:
- Article
47
Dynamics of gas turbine engines rotors taking into account non-linear effects.
- Published in:
- Vibroengineering Procedia, 2016, v. 8, p. 361
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- Publication type:
- Article
48
Differential evolution applied to parameter estimation of induction motor.
- Published in:
- Archives of Control Sciences, 2009, v. 19, n. 1, p. 59
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- Publication type:
- Article
49
Development of an intermittency transport equation for modeling bypass, natural and separation-induced transition.
- Published in:
- Journal of Turbulence, 2021, v. 22, n. 9, p. 562, doi. 10.1080/14685248.2021.1932947
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- Article
50
DETERMINING THE INFLUENCE OF COMPRESSOR FLOW PATH ABRASIVE WEAR ON THE GAS TURBINE ENGINE CHARACTERISTICS.
- Published in:
- Eastern-European Journal of Enterprise Technologies, 2023, v. 122, n. 1, p. 12, doi. 10.15587/1729-4061.2023.275546
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- Publication type:
- Article