| Sl. No. |
Sponsoring Agency |
Project Title |
Duration |
| 1. |
Aeronautics
Research and Development Board, Propulsion Panel |
Active
boundary layer control in 2-D cascade and axial flow fan |
2006-2008 |
| 2. |
Aeronautics
Research and Development Board, Propulsion Panel |
Axial
fan performance evaluation and enhancement strategies
under static and dynamic
inflow distortions |
2008-2010 |
| 3. |
Siemens
Energy Inc., Florida, USA |
Annular
Turbine Diffuser Aerodynamics |
2008-2013 |
| 4. |
Pratt and
Whitney, Canada |
Tip Flow
in High Hub-tip Ratio Axial Flow Compressors |
2009-2012 |
| 5. |
Aeronautics
Research and Development Board, Propulsion Panel |
Parametric study of contra-rotating
axial flow fans under different inflow conditions and
design modifications based on the parametric study |
2012-2014 |
| 6. |
Aeronautical
Development Agency |
Flow
characteristics, active and passive flow control in a
serpentine intake duct |
2011-2014 |
7.
|
Aeronautics Research and
Development Board, Aerodynamics Panel |
Investigation of secondary flow
and its control in an axial compressor cascade with and
without tip gap |
2013-2015
|
8.
|
Defence Research and
Development Organization
|
Effect of inflow distortion on
fan performance
|
2017-2020
|
9.
|
Defence Research and
Development Organization |
Losses in a fan-booster duct
|
2017-2020
|
10.
|
Defence Research and
Development Organization |
Design and analysis of a mixed
flow compressor
|
2017-2020
|
