Works matching DE "AIRPLANE compressors"
Results: 10
YÜKSEK BYPASSLI TURBOFAN MOTORLARININ TASARIM NOKTASI ANALİZLERİ.
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- Journal of Aeronautics & Space Technologies / Havacilik ve Uzay Teknolojileri Dergisi, 2008, v. 3, n. 3, p. 1
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- Article
THE NOZZLE GUIDE VANE PROBLEM.
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- Operations Research, 1988, v. 36, n. 1, p. 18, doi. 10.1287/opre.36.1.18
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The Impact of Volute Aspect Ratio on the Performance of a Mixed Flow Turbine.
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- Aerospace (MDPI Publishing), 2017, v. 4, n. 4, p. 56, doi. 10.3390/aerospace4040056
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Fatigue Reliability Analysis of a Compressor Disk Based on Probability Cumulative Damage Criterion.
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- Materials (1996-1944), 2020, v. 13, n. 9, p. 2182, doi. 10.3390/ma13092182
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Qualification Approach of a High-Pressure Compressor Drum of a Military Turbofan Engine for Structural Integrity and Life.
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- Journal of Failure Analysis & Prevention, 2015, v. 15, n. 4, p. 503, doi. 10.1007/s11668-015-9963-2
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- Article
Overview of low emission combustors of aircraft turbine drive units.
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- Combustion Engines (2300-9896), 2020, v. 183, n. 4, p. 45, doi. 10.19206/CE-2020-407
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REVIEW OF HOW AERO ENGINES WORK.
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- Technical Journal / Tehnički Glasnik, 2015, v. 9, n. 4, p. 381
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Effects of pre-oxidation on the corrosion behavior of pure Ti under coexistence of solid NaCl deposit and humid oxygen at 600 °C: the diffusion of chlorine.
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- Scientific Reports, 2020, v. 10, n. 1, p. N.PAG, doi. 10.1038/s41598-020-73034-y
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- Article
MATHEMATICAL MODEL FOR A JET ENGINE WITH COOLING FLUID INJECTION INTO ITS COMPRESSOR.
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- Scientific Research & Education in the Air Force - AFASES, 2014, v. 1, p. 265
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Effect of thermal exposure on degradation of compressor blades in aero-jet engines.
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- Corrosion Engineering, Science & Technology, 2015, v. 50, n. 4, p. 283, doi. 10.1179/1743278214Y.0000000223
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- Article