Compressible and incompressible fluid seals: Influence on rotordynamic response and stability

التفاصيل البيبلوغرافية
العنوان: Compressible and incompressible fluid seals: Influence on rotordynamic response and stability
المؤلفون: Thames, Howard D.
المصدر: CASI
سنة النشر: 1992
المجموعة: NASA Technical Reports Server (NTRS)
مصطلحات موضوعية: MECHANICAL ENGINEERING
جغرافية الموضوع: Unclassified, Unlimited, Publicly available
الوصف: The flow field inside a whirling annular seal operating a Reynolds numbers of 12,000 and 24,000 and a Taylor number of 6,600 was measured. The rotor was mounted eccentric (50 percent) upon the facilities shaft which resulted in a circular orbit at a whirl ratio of 1.0. Three papers which summarize the work were written and are presented. Addition measurements were performed for the annular seal operating at an eccentricity ratio of 10 percent for Re = 24,000 and Ta = 6,600. A labyrinth seal was also installed into the facility and operated at an eccentricity ratio of 50 percent at the same Reynolds and Taylor numbers. These data are currently being reduced and analyzed.
نوع الوثيقة: other/unknown material
وصف الملف: application/pdf
اللغة: unknown
العلاقة: Document ID: 19930001703; Accession ID: 93N10891; http://hdl.handle.net/2060/19930001703Test
الإتاحة: http://hdl.handle.net/2060/19930001703Test
حقوق: No Copyright
رقم الانضمام: edsbas.CE7B8DCC
قاعدة البيانات: BASE