त्वरित संपर्क
Anshul Khandelwal
Department: वांतरिक्ष अभियांत्रिकी
Research Topic
The topic of my research is flow past an airfoil oscillating asymmetrically in pitching motion. The effect of different parameters such as mean angle, amplitude, non-dimensional reduced frequency, Reynolds number, and the degree of asymmetry in this asymmetric sinusoidal motion is investigated using unsteady pressure measurement and PIV, particularly at high reduced frequencies.
शिक्षा
M.Tech.: IIT Kanpur, 2010
B.Tech.: IIT Kanpur, 2008
चयनित प्रकाशन
"Studies on tab controls on subsonic co-flow jets", Pradeep Arora, Anshul Khandelwal, K.L. Narayana & E Rathakrishnan, 2nd International Conference on Recent Advances in Experimental Fluid Mechanics, 2008.
Pradeep Arora, Anshul Khandelwal, and E Rathakrishnan, Studies on Tab Controls on Subsonic and Sonic Co-Flow Jets Paper Number: AIAA-2008-3509, 27th AIAA Applied Aerodynamics, San Antonio, Texas, 22-25 June 2009
"Experimental Investigation Of Asymmetric Pitching Oscillations Of A Symmetric Airfoil", Anshul Khandelwal, K.Poddar and D.Das, Aerospace Students Doctoral Students Symposium, 2014.
पुरस्कार एवं फैलोशिप
Academic Excellence award for the year 2008-09
NSTSE scholar in IXth & Xth standards