Zobrazeno 1 - 10
of 13
pro vyhledávání: '"Janaki Rami Reddy Mudipalli"'
Autor:
DilipkumarBhanudasji Alone, S. Satish Kumar, Shobhavathy M. Thimmaiah, Janaki Rami Reddy Mudipalli, A.M. Pradeep, Srinivasan Ramamurthy, Venkat S. Iyengar
Publikováno v:
Propulsion and Power Research, Vol 5, Iss 3, Pp 236-249 (2016)
This paper presents the experimental results to understand the performance of moderately loaded high speed single stage transonic axial flow compressor subjected to various configurations of axial extensions of bend skewed casing treatment with moder
Externí odkaz:
https://doaj.org/article/815d70029fbe4396911147c7c1bd22f4
Autor:
Dilipkumar Bhanudasji Alone, S. Satish Kumar, Shobhavathy M. Thimmaiah, Janaki Rami Reddy Mudipalli, A. M. Pradeep, Srinivasan Ramamurthy, Venkat S. Iyengar
Publikováno v:
International Journal of Rotating Machinery, Vol 2014 (2014)
This paper presents experimental results of a single stage transonic axial flow compressor coupled with low porosity bend skewed casing treatment. The casing treatment has a plenum chamber above the bend slots. The depth of the plenum chamber is vari
Externí odkaz:
https://doaj.org/article/9ffa5768e4f44369a78d0608f5d29dd0
Autor:
S. Satish Kumar, Dilipkumar Bhanudasji Alone, Shobhavathy M. Thimmaiah, Janaki Rami Reddy Mudipalli, Lakshya Kumar, Soumendu Jana, S. B. Kandagal, Ranjan Ganguli
Publikováno v:
Journal of Turbomachinery. 144
For successful implementation of casing treatment designs in axial compressors, apart from the stall margin improvement benefits, aeroelasticity also plays a major role. This manuscript addresses the not often discussed aeroelastic aspects of a new d
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::522201513bbe23a5de0d7fb881e6974b
https://doi.org/10.1115/1.4053385
https://doi.org/10.1115/1.4053385
Autor:
Shobhavathy M. Thimmaiah, S. Satish Kumar, Ranjan Ganguli, Soumendu Jana, Dilipkumar Bhanudasji Alone, S. B. Kandagal, Lakshya Kumar, Janaki Rami Reddy Mudipalli
Publikováno v:
Aerospace Science and Technology. 112:106587
In this manuscript, a new discrete type of passive Self-Recirculating Casing Treatment (RCT) is designed for a transonic axial compressor stage, fabricated, and tested for its performance. Parametric evaluation of the casing flush-mounted RCT for inj
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::73635baa4e2d263c40b56678a6bcdc21
https://doi.org/10.1016/j.ast.2021.106587
https://doi.org/10.1016/j.ast.2021.106587
Autor:
Dilipkumar Bhanudasji Alone, Venkat S. Iyengar, M.T. Shobhavathy, Srinivasan Ramamurthy, Satish Kumar, Janaki Rami Reddy Mudipalli, A. M. Pradeep
Publikováno v:
IndraStra Global.
Development of casing treatment geometries which will enhance the stable operating envelope of the compressor stage without sacrificing the efficiency is a great challenge for the designers. Bend skewed casing treatment with relatively lower porositi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::fc1c536f633b9d8186f5b3516afd7abf
Autor:
Janaki Rami Reddy Mudipalli, Srinivasan Ramamurthy, A. M. Pradeep, Dilipkumar Bhanudasji Alone, Shobhavathy M. Thimmaiah, Satish Kumar, Venkat S. Iyengar
Publikováno v:
International Journal of Rotating Machinery, Vol 2014 (2014)
This paper presents experimental results of a single stage transonic axial flow compressor coupled with low porosity bend skewed casing treatment. The casing treatment has a plenum chamber above the bend slots. The depth of the plenum chamber is vari
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d6b13db246879fb103a020dfc1575860
https://doi.org/10.1155/2014/625876
https://doi.org/10.1155/2014/625876
Autor:
Ranjan Ganguli, Soumendu Jana, S. Satish Kumar, Janaki Rami Reddy Mudipalli, Dilipkumar Bhanudasji Alone, Shobhavathy M. Thimmaiah, S. B. Kandagal
Publikováno v:
ASME 2014 Gas Turbine India Conference.
Detailed steady and unsteady experimental measurements and analysis were performed on a Single stage Transonic Axial Compressor with asymmetric rotor tip clearance for studying the compressor stall phenomena. The installed compressor had asymmetric t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e30919272b48150d4d9ef6d232157773
https://doi.org/10.1115/gtindia2014-8167
https://doi.org/10.1115/gtindia2014-8167
Autor:
A. M. Pradeep, Srinivasan Ramamurthy, Janaki Rami Reddy Mudipalli, Shobhavathy M. Thimmaiah, Venkat S. Iyengar, Subramani Satish Kumar, Dilipkumar Bhanudasji Alone
Publikováno v:
Web of Science
A bend skewed casing treatment was designed, to study the influence of one of its geometrical parameter porosity on the stable performance of single stage transonic axial flow compressor. The compressor was designed for the stage total-to-total press
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::5c4357a79ffd784288a27f1d872f2739
https://doi.org/10.1115/gt2014-26102
https://doi.org/10.1115/gt2014-26102
Autor:
Venkat S. Iyengar, Dilipkumar Bhanudasji Alone, Subramani Satish Kumar, A. M. Pradeep, Shobhavathy M. Thimmaiah, Srinivasan Ramamurthy, Janaki Rami Reddy Mudipalli
Publikováno v:
Web of Science
The performance of an aero-engines to a large extend depends on the performance behavior of axial flow compressors and is restricted by the compressor instabilities like rotating stall and surge. In the present study, attempts have been made to desig
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::84ca2a975519db7ab64da552c0c8cade
https://doi.org/10.1115/gt2014-26099
https://doi.org/10.1115/gt2014-26099
Autor:
Dilipkumar Bhanudasji Alone, Venkat S. Iyengar, Janaki Rami Reddy Mudipalli, Subramani Satish Kumar, Shobhavathy M. Thimmaiah, Srinivasan Ramamurthy, A. M. Pradeep
Publikováno v:
Web of Science
This paper describes the study of flow behavior of the transonic compressor stage in un-stalled and stalled conditions. Experiments were carried out in an open circuit single stage transonic axial flow compressor test rig. The test compressor was des
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f8f8edcf01cb9a97e18ef619329057b6
https://doi.org/10.1115/gtindia2013-3620
https://doi.org/10.1115/gtindia2013-3620