Recent content by chinmay

  1. chinmay

    Handling Rotational Degrees of Freedom in Coordinate Transformations

    I am trying to analyse response of a dynamic system. The source disturbance is about x,y,theta (rotation about x ) & Phi of one coordinate system (red coloured coordinate system in the attached figure). I need to get the response in another coordinate system ( green coloured coordinate system...
  2. chinmay

    Simulation of Dynamic Charateristics

    Thanks for your response. The sides of the panel is approximately 800 mm. During testing accelerometer was put at 4 locations on the panel. In my FE model, I gave the same input force as that in testing and checked the response at the location of accelerometer, (exact location was not known, so...
  3. chinmay

    Simulation of Dynamic Charateristics

    ok, I have experimental data upto 120 Hz only, in which only first mode is captured. I will try to model the complete structure. Thanks for the reply
  4. chinmay

    Simulation of Dynamic Charateristics

    Sir, the complete cuboid is ~ 1000 kg, whereas top panel assembly is only ~62 kg. The systems mounted on top deck are highly stiff (frequency >1Khz). So my idea is to make FE model of only top deck (instead of complete structure) for analysis, but this top deck model must have same dynamic...
  5. chinmay

    Simulation of Dynamic Charateristics

    I have an assembly (a cuboid shaped structure). The vibration test data of this structure is available with me. I want to study the effect of vibration generated by a system mounted on top panel on another system mounted on same top panel. In order to complete this, I have prepared the FE model...
  6. chinmay

    Exploring Vibration Isolation and Structural Dynamics in Aerospace Engineering

    Hello , I am Chinmay Rajhans, pursuing my M.tech in Aerospace Engg. My area of interest in Vibration isolation and structural dynamics
  7. chinmay

    Torsional Vibration of Rotor-Shaft

    I have developed a mathematical model to study the dynamic behavior of rotor (with 6 dof). It is assumed that rotor is rigidly mounted at the mid point of shaft, and both end of the shaft is attached to ball bearing. I have developed the FE model for it too, and the frequencies in X, Y, Theta...
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