Follow
Dr.Dilipkumar Bhanudasji Alone
Dr.Dilipkumar Bhanudasji Alone
Senior Principal Scientist
Verified email at nal.res.in
Title
Cited by
Cited by
Year
Aerodynamic characterization of a transonic axial flow compressor stage–with asymmetric tip clearance effects
SS Kumar, DB Alone, SM Thimmaiah, JRR Mudipalli, R Ganguli, ...
Aerospace Science and Technology 82, 272-283, 2018
302018
Aerodynamic behavior of a transonic axial flow compressor stage with self-recirculating casing treatment
SS Kumar, DB Alone, SM Thimmaiah, JRR Mudipalli, L Kumar, R Ganguli, ...
Aerospace Science and Technology 112, 106587, 2021
252021
Experimental assessment on effect of lower porosities of bend skewed casing treatment on the performance of high speed compressor stage with tip critical rotor characteristics
DB Alone, SS Kumar, MT Shobhavathy, JRR Mudipalli, AM Pradeep, ...
Aerospace Science and Technology 60, 193-202, 2017
222017
Performance characterization of the effect of axial positioning of bend skewed casing treatment retrofitted to a transonic axial flow compressor
DB Alone, SS Kumar, S Thimmaiah, JRR Mudipalli, AM Pradeep, ...
Turbo Expo: Power for Land, Sea, and Air 45608, V02AT37A026, 2014
17*2014
Improvement of moderately loaded transonic axial compressor performance using low porosity bend skewed casing treatment
DB Alone, SS Kumar, SM Thimmaiah, JRR Mudipalli, AM Pradeep, ...
International Journal of Rotating Machinery 2014, 2014
172014
Stability management of high speed axial flow compressor stage through axial extensions of bend skewed casing treatment
DB Alone, SS Kumar, SM Thimmaiah, JRR Mudipalli, AM Pradeep, ...
Propulsion and Power Research 5 (3), 236-249, 2016
102016
On understanding the effect of plenum chamber of a bend skewed casing treatment on the performance of a transonic axial flow compressor
DB Alone, SS Kumar, S Thimmaiah, JRR Mudipalli, AM Pradeep, ...
Turbo Expo: Power for Land, Sea, and Air 45608, V02AT37A028, 2014
102014
Numerical investigations on influence of uniform blade surface roughness on the performance characteristics of a transonic axial flow compressor stage
RJ Chotalia, DB Alone
Gas Turbine India Conference 58509, V001T01A008, 2017
82017
Aeroelastic aspects of axial compressor stage with self-recirculating casing treatment
SS Kumar, DB Alone, SM Thimmaiah, JRR Mudipalli, L Kumar, S Jana, ...
Journal of Turbomachinery 144 (6), 061008, 2022
62022
Experimental Investigation of Unsteady Flow in a Transonic Uni-Stage Axial Compressor
SS Kumar, DB Alone, SM Thimmaiah, JRR Mudipalli, R Ganguli, ...
Gas Turbine India Conference 49644, V001T01A005, 2014
62014
Stall margin improvement of a single stage transonic axial flow compressor using naturally aspirated slots
HK Borra, DB Alone
Gas Turbine India Conference 57311, V001T01A005, 2015
42015
Evolution of unsteady secondary flow structures near the onset of stall in a tip-critical transonic axial flow compressor stage
L Kumar, DB Alone, AM Pradeep
Physics of Fluids 35 (10), 2023
32023
Profile loss investigations with a S-CO2 axial turbine aerofoil
RS Kumaran, DB Alone, P Kumar
Turbo Expo: Power for Land, Sea, and Air 84232, V011T31A015, 2020
32020
Aerodynamics of inter-spool duct under the influence of an upstream transonic compressor stage
L Kumar, DB Alone, AM Pradeep
Aerospace Science and Technology 137, 108282, 2023
22023
Influence of an upstream transonic axial compressor stage on the performance of inter-stage duct
L Kumar, DB Alone, AM Pradeep
Journal of Mechanical Science and Technology 37 (5), 2179-2185, 2023
22023
Preliminary Aerodynamic Design of a S-CO2 Axial Turbine
RS Kumaran, DB Alone, A Nassar, P Kumar
Gas Turbine India Conference 85536, V001T12A009, 2021
22021
NUMERICALLY UNDERSTAND THE COMBINED EFFECT OF TIP CLEARANCE AND CIRCUMFERENTIAL GROOVES CASING TREATMENT ON THE PERFORMANCE OF SINGLE STAGE TRANSONIC AXIAL FLOW COMPRESSOR
Mitesh Goswami,Dr.Dilipkumar Bhanudasji Alone, Harish S Choksi
Proceedings of the ASME 2015 Gas Turbine India Conference GTINDIA2015 …, 2015
2*2015
Numerical studies on effect of stepped tip clearance height on the performance of single stage transonic axial flow compressor
P Batabyal, DB Alone, SK Maharana
Gas Turbine India Conference 35161, V001T01A017, 2013
22013
M.: Flow behavior in a single stage transonic axial flow compressor with diminishing to large rotor tip clearances in the presence of axisymmetric circumferential grooved …
M Goswami, D Alone, M Inoue, M Kuroumaru, S Yoshida, T Minami, ...
Proceedings of the Asian Congress on Gas Turbines, ACGT2016-03, IITB, Mumbai …, 2016
12016
COMPUTATIONAL ANALYSIS OF EFFECT OF CIRCUMFERENTIAL GROOVE CASING TREATMENT WITH DIFFERENT AXIAL COVERAGE OVER ROTOR BLADE TIP CHORD ON THE PERFORMANCE OF A TRANSONIC AXIAL …
Nishit Mehta,Dr.Dilipkumar Bhanudasji Alone, Harish Choksi
Proceedings of the ASME 2015 Gas Turbine India Conference,GTINDIA2015 …, 2015
1*2015
The system can't perform the operation now. Try again later.
Articles 1–20