Works matching DE "AIR intakes (Jet engines)"
Results: 20
Aerodynamic Testing of Helicopter Side Intake Retrofit Modifications.
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- Aerospace (MDPI Publishing), 2017, v. 4, n. 3, p. 33, doi. 10.3390/aerospace4030033
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THERMAL ENGINE AIR INTAKE SYSTEM.
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- Journal of Industrial Design & Engineering Graphics, 2018, v. 13, n. 1, p. 13
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FORMING/PROCESSING.
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- Advanced Materials & Processes, 2004, v. 162, n. 10, p. 22
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- Article
FSI STUDY OF THE EFFECT OF AIR INLET/OUTLET ARRANGEMENTS ON THE RELIABILITY AND COOLING PERFORMANCES OF FLEXIBLE PRINTED CIRCUIT BOARD ELECTRONICS.
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- Journal of Thermal Science & Technology / Isı Bilimi ve Tekniği Dergisi, 2013, v. 33, n. 1, p. 43
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- Article
Cowl Deflection Angle in a Supersonic Air Intake.
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- Defence Science Journal, 2009, v. 59, n. 2, p. 99, doi. 10.14429/dsj.59.1496
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Development of Eddy Current Test Procedure for Non-destructive Detection of Fatigue Cracks and Corrosion in Rivets of Air-intake Structures.
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- Defence Science Journal, 2009, v. 59, n. 2, p. 106, doi. 10.14429/dsj.59.1497
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- Article
Measurement of Total Water with a Tunable Diode Laser Hygrometer: Inlet Analysis, Calibration Procedure, and Ice Water Content Determination.
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- Journal of Atmospheric & Oceanic Technology, 2007, v. 24, n. 3, p. 463, doi. 10.1175/JTECH1975.1
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Assessment of unsteady-RANS approach against steady-RANS approach for predicting twin impinging jets in a cross-flow.
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- Cogent Engineering, 2014, v. 1, n. 1, p. 1, doi. 10.1080/23311916.2014.936995
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LOW-PRESSURE REVERSIBLE AXIAL FAN DESIGNED WITH DIFFERENT SPECIFIC WORK OF ELEMENTARY STAGES.
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- Thermal Science, 2012, v. 16, p. S605, doi. 10.2298/TSCI120503195B
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The Effect of Carbon Dioxide in Non-Air Inlet Mixture on Combustion Performance in Diesel Engine.
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- International Review of Mechanical Engineering, 2009, v. 3, n. 6, p. 788
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Comparison of Leakage Performance in Three Types of Gas Annular Seals Operating at a High Temperature (300°C).
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- Tribology Transactions, 2010, v. 53, n. 3, p. 463, doi. 10.1080/10402000903420803
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Acoustic attenuation performance of a perforated resonator with a multi-chamber and its optimal design.
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- Noise & Vibration Worldwide, 2015, v. 46, n. 8, p. 27
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- Article
Relationship Model Between Recrystallization Critical Stress and Structure Designed Parameters on Single Crystal Turbine Blade.
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- Journal of Nanjing University of Aeronautics & Astronautics / Nanjing Hangkong Hangtian Daxue Xuebao, 2014, v. 46, n. 6, p. 909
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Aerodynamic design and experimental modelling of an innovative supersonic three-dimensional air-intake.
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- Aeronautical Journal, 2013, v. 117, n. 1192, p. 559, doi. 10.1017/S0001924000008216
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Investigation of the Flow Structure in a Model Scramjet Air Intake with Transverse Hydrogen Fuel Injection into Supersonic Crossflow.
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- Fluid Dynamics, 2021, v. 56, n. 3, p. 334, doi. 10.1134/S0015462821030083
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Leading edge bluntness effect on the flow in a model air-inlet.
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- Fluid Dynamics, 2014, v. 49, n. 4, p. 454, doi. 10.1134/S0015462814040061
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On the possible formation of a vortex flow in a supersonic inlet with three-dimensional compression.
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- Fluid Dynamics, 2006, v. 41, n. 4, p. 649, doi. 10.1007/s10697-006-0084-1
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Modelling of Electromagnetic Scattering from Large and General Intakes on Complex Platforms.
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- Applied Computational Electromagnetics Society Journal, 2018, v. 33, n. 7, p. 802
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Discontinuous Galerkin Time Domain Method for Scattering Analysis of Air-Inlets.
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- Applied Computational Electromagnetics Society Journal, 2013, v. 28, n. 6, p. 479
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Investigation of the impact of imposed air inlet velocity oscillations on the formation and oxidation of soot using simultaneous 2-Colour-TIRE-LII.
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- Applied Physics B: Lasers & Optics, 2015, v. 119, n. 4, p. 777, doi. 10.1007/s00340-015-6117-x
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- Article