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Kumar Vikram Singh
Kumar Vikram Singh
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Title
Cited by
Cited by
Year
Modern applications of nanotechnology in textiles
APS Sawhney, B Condon, KV Singh, SS Pang, G Li, D Hui
Textile Research Journal 78 (8), 731-739, 2008
3872008
Effect of fiber orientation on the structural behavior of FRP wrapped concrete cylinders
G Li, D Maricherla, K Singh, SS Pang, M John
Composite structures 74 (4), 475-483, 2006
1272006
Buckling of functionally graded and elastically restrained non-uniform columns
KV Singh, G Li
Composites Part B: Engineering 40 (5), 393-403, 2009
1052009
Transcendental eigenvalue problem and its applications
KV Singh, YM Ram
AIAA journal 40 (7), 1402-1407, 2002
682002
Receptance-based active aeroelastic control using multiple control surfaces
KV Singh, LA McDonough, R Kolonay, JE Cooper
Journal of Aircraft 51 (1), 335-342, 2014
492014
Free vibration and physical parameter identification of non-uniform composite beams
KV Singh, G Li, SS Pang
Composite structures 74 (1), 37-50, 2006
492006
Pole assignment using state feedback with time delay in friction-induced vibration problems
KV Singh, H Ouyang
Acta Mechanica 224 (3), 645-656, 2013
422013
Eigenvalue and eigenvector computation for discrete and continuous structures composed of viscoelastic materials
KV Singh
International Journal of Mechanical Sciences 110, 127-137, 2016
372016
Receptance-based active aeroelastic control with embedded control surfaces having actuator dynamics
KV Singh, RN Brown, R Kolonay
Journal of Aircraft 53 (3), 830-845, 2016
372016
Transcendental inverse eigenvalue problems in damage parameter estimation
KV Singh
Mechanical Systems and Signal Processing 23 (6), 1870-1883, 2009
342009
Partial eigenvalue assignment and its stability in a time delayed system
KV Singh, R Dey, BN Datta
Mechanical Systems and Signal Processing 42 (1-2), 247-257, 2014
332014
Dynamic absorption by passive and active control
KV Singh, YM Ram
J. Vib. Acoust. 122 (4), 429-433, 2000
272000
Active aeroelastic output feedback control with partial measurements by the method of receptances
KV Singh, C Black, R Kolonay
Aerospace Science and Technology 86, 47-63, 2019
262019
Active aeroelastic control using the receptance method
KV Singh, LA McDonough, J Mottershead, J Cooper
ASME International Mechanical Engineering Congress and Exposition 44458, 137-146, 2010
242010
Active aeroelastic control with time delay for targeted flutter modes
KV Singh
Aerospace science and technology 43, 281-288, 2015
232015
Developing predictive tools for friction stir weld quality assessment
KV Singh, C Hamilton, S Dymek
Science and technology of welding and joining 15 (2), 142-148, 2010
192010
Revitalizing the engineering curriculum through studio based instruction
F Khan, N Birchfield, KV Singh
ASME International Mechanical Engineering Congress and Exposition 45219, 131-138, 2012
172012
Flutter control using vibration test data: theory, rig design and preliminary results
E Papatheou, X Wei, S Jiffri, M Prandina, MG Tehrani, S Bode, KV Singh, ...
ISMA international conference on noise and vibration engineering, Leuven …, 2012
172012
Effect of laminated core on rotor mode shape of large high speed induction motor
S Singhal, KV Singh, A Hyder
2011 IEEE International Electric Machines & Drives Conference (IEMDC), 1557-1562, 2011
172011
Quadratic partial eigenvalue assignment problem with time delay for active vibration control
JM Pratt, KV Singh, BN Datta
Journal of Physics: Conference Series 181 (1), 012092, 2009
172009
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