ISSN (Online) : 2319 - 6734 ISSN (Print) : 2319 - 6726
Special Issue
National Conference on "Advances In Modelling And Analysis Of Aerodynamic Systems" |
Articles:
Conference Objective |
Identification of airfoil sections with improved aerodynamic characteristics |
File Size | 497 KB |
Diagnosis of Modal Characteristics of Aircraft Wing Model subjected to Irregularities |
Deepak K. Agarwalla, Dayal R. Parhi | File Size | 319 KB |
Frequency Response of Composite Laminates at Various Boundary Conditions |
File Size | 470 KB |
Vibration Analysis of a Non Rotating Beam with breathing crack |
File Size | 469 KB |
Effect of Parameters in Power Harvesting From Piezoaeroelastic System |
File Size | 648 KB |
Computational Aerodynamic Analysis on Store Separation from Aircraft using Pylon |
File Size | 380 KB |
Aeroelasticity Consideration in Aerodynamic Adaptation of Wing |
File Size | 818 KB |
Replacement of Nab Propeller Blade with Composite for Strength Criteria |
File Size | 535 KB |
Dynamic Analysis of Cracked Rotor-Bearing System With Fractional-Order Damping |
File Size | 310 KB |
Computational Study on Effects of Shockwave on Combustion and Injected FuelBy Unconventional Positioning of Injectors |
File Size | 509 KB |
Analysis of Cantilever beams in Liquid Media: A case study of a microcantilever |
File Size | 364 KB |
Study of fault in outer race of Roller Bearings using Acoustic emission and Vibration analysis |
File Size | 668 KB |
Experimental Investigation to Study Flow & Heat Transfer Characteristics over A NACA0018 Aerofoil |
M .Sri Rama Murthy, A.V.S.S.K.S.Gupta | File Size | 261 KB |
Finite element analysis of ultrasonic vibratory tool and experimental study in ultrasonic vibration-assisted Turning (uvt) |
File Size | 441 KB |
Optimum Material Evaluation of Fan Blades Using Reverse Engineering Approach |
File Size | 675 KB |
Free Vibration Analysis of Laminated Composite Cylindrical Panels |
File Size | 496 KB |
Damping measurement in composite materials using combined finite element and frequency response method |
File Size | 964 KB |
Modal Analysis of Damped Rotor using Finite Element Method |
File Size | 560 KB |