Zobrazeno 1 - 4
of 4
pro vyhledávání: '"A. N. Vishwanatha Rao"'
Autor:
Mangalanathan Umapathy, Anagha S. Nambiar, G. Uma, A. N. Vishwanatha Rao, T. N. Satish, V. P. S. Naidu, Soumemndu Jana
Publikováno v:
Proceedings of the National Aerospace Propulsion Conference ISBN: 9789811550386
Developmental testing of gas turbine propulsion systems involves iterative experimental studies right from First Engine to Test (FETT) till production release. During initial design validation tests, engines require dedicated instrumentation for carr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8e199b109e9bfc39afb3a27d788e99bc
https://doi.org/10.1007/978-981-15-5039-3_16
https://doi.org/10.1007/978-981-15-5039-3_16
Publikováno v:
Proceedings of the National Aerospace Propulsion Conference ISBN: 9789811550386
Rotor blade vibration in turbomachinery has been a major cause of failure due to HCF, often resulting in catastrophic damage. The primary aeromechanical design concerns are blade flutter and forced vibration that need to be quantified. The severity o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0bf995a88998618dc833f5ef41a9ea5b
https://doi.org/10.1007/978-981-15-5039-3_15
https://doi.org/10.1007/978-981-15-5039-3_15
Publikováno v:
Lecture Notes in Electrical Engineering ISBN: 9789811555572
With the advancement in Modeling and Simulation technology, an integrated approach of incorporating the concept of Early Integration Engineers Involvement (EIEI) during developmental aero engine control system design process and the Controller-In-the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::81672ff1b7ddd576882a59df07885e41
https://doi.org/10.1007/978-981-15-5558-9_74
https://doi.org/10.1007/978-981-15-5558-9_74
Autor:
A. N. Vishwanatha Rao, O. N. Ramesh
Publikováno v:
Sadhana. 32:43-49
In air-compression systems, instabilities occur during operation close to their peak pressure-rise capability. However, the peak efficiency of a compression system lies close to this region of instability. A surge is a violent mode of instability whe