IISc Bangalore

S. B. Kandagal

Principal Research Scientist
Structures
Email: ksb[at]iisc.ac.in
Office Phone Number: +91-80-22933018
Lab Phone Number: +91-80-22933151
Office Room Number: AE031
Lab Room Number : AE009

 

Education

Ph.D,  Indian Institute of Science (2005)
M.Tech, NITK, Suratkal (1992 )
B.E,  NITK, Suratkal (1989)

Research Interests

  • Structural mechanics, Vibration and noise control, Smart Structures,
  • Experimental Modal analysis, structural optimisation of Mechanical systems

Research Statement

  • Structural mechanics, Vibration and noise control, smart structures,
  • Experimental Modal analysis, structural optimisation of Mechanical systems
  1. Vadiraj B, M ABharadwaj, Omkar SN, Kandagal SB. Dynamic responses of human body during aircraft seat ejection. In 28th National Convention of Aerospace Engineers and National Seminar. 2014
  2. Kumar SS, Alone DB, Shubhavathy MT, , Ganguli R, Kandagal SB, et al. Experimental Investigation of Unsteady Flow in a Transonic Unistage Axial Compressor. In ASME 2014 Gas Turbine India Conference. New Delhi, India; 2014. 2014
  3. Vadiraj B, Omkar SN, Kandagal SB, Kiran MC. Human response characteristics to impact conditions during spacecraft takeoff and impact landing. International journal of Aerospace innovations. 2012;Volume 4. 2012
  4. Vadiraj B, Omkar SN, Kandagal SB. Acceleration responses at different body segments and selected body orientations to spacecraft takeoff and impact landing. In 1. MSC Software India User Conference, September 2012. 2012
  5. Kandagal SB, Venkatraman K. Flutter control using Resistively Shunted Piezoceramics. The Aeronautical Journal of the Royal Aeronautical Society. 2010;114(1156). 2010
  6. Giri K, Kandagal SB. Form with displacable vibratory panel. US 6939121. 2005
  7. Kandagal SB, Venkatraman K. Form factors for vibration control of beams using resistively shunted piezoceramics. The Journal of Sound and Vibration. 2004;274. 2004
  8. Kandagal SB, Venkatraman K. Closed loop flutter control using strain actuation. The Aeronautical Journal of the Royal Aeronautical Society. 2004;108(1083). 2004

This will be updated soon.

 

 

This will be updated soon.