Impact Data Analysis and Sensor Modification for Pressure Data of Granular Gases in Reduced Gravity - PowerPoint PPT Presentation

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Impact Data Analysis and Sensor Modification for Pressure Data of Granular Gases in Reduced Gravity

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Frequency Dead Spots at 150 Hz multiples. Time Series Analysis ... Dr. Michael Wilson -- National Academy of Sciences. Mr. Shawn Jackson -- University of Tulsa ... – PowerPoint PPT presentation

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Title: Impact Data Analysis and Sensor Modification for Pressure Data of Granular Gases in Reduced Gravity


1
Impact Data Analysis and Sensor Modification for
Pressure Data of Granular Gases in Reduced
Gravity
  • Aaron Coyner, Justin Mitchell, and Matthew Olson
  • University of Tulsa
  • April 9, 2003

2
Granular Gases
  • Excited granular media can simulate molecules
    similar to those in ideal gases
  • Excitation results in kinetic motion
  • Velocities have distribution of amplitudes
  • Random directions
  • Modified gas laws can be applied
  • Granular Temperature
  • Theory shows v2 proportionality
  • Granular Pressure
  • One experiment shows v3/2 proportionality
  • Theory predicts ordering (inelastic collapse)

A. Puglisi, A. Baldassarri, and V. Loreto,
Phys. Rev E 66 061305.
É. Falcon et al. , Phys. Rev. Lett. 80. 440
(1999).
3
Importance of Impact Data
  • Impact data can aid in development of speed
    distributions.
  • Can apply results to large systems of particles
    without individual tracking
  • Each experiment set should have a distinct set of
    collision frequencies
  • Frequency response should depend on number of
    particles and driving parameters.
  • Data should also reflect the predicted collapse
    if it occurs

4
Relevance to Reduced Gravity
  • Inelastic Collapse of granular systems in reduced
    gravity could explain
  • Asteroid Formation
  • Planetary Rings
  • Other celestial systems that could not for by
    gravitation alone.

5
Ways to Achieve Reduced Gravity
  • Sounding Rocket
  • Falcon et al. (1999)
  • Nasas KC-135 Weightless Wonder
  • Space Shuttle Flight
  • Get Away Special

KC-135
6
The Gr.A.I.N.S. Experiment
  • Box set of 8 sample cells
  • Each cell 1 in3
  • Each cell contain varied number of brass ball
  • Sapphire walls
  • Each cell has an impact sensor
  • Impact data stored in external data drive
  • Mechanical Shaker System
  • Varies amplitude and frequency
  • Cameras and Mirrors
  • Cameras record video of 3 faces of the cube.

7
Impact Sensors (Initial Run)
  • 0.75 diameter
  • APC 850 ceramic piezoelectric material
  • lead zirconate titanate formulation
  • 2 MHz Bandwidth
  • Wired into Camera Audio Channels
  • Subminiature coax used

Piezoelectric Disk
8
Steps in Data Analysis
  • Determine camera effects
  • Amplification of signal
  • Signal coupling (unexpected)
  • 300 mV signal on right channel appears on left
    channel with equal amplitude at gt 600 Hz
  • Initial run of time series and power spectra
  • FFT analysis
  • Low frequency and high frequency responses
  • Audio parsing to obtain low frequency peaks
    evident in time series

9
Camera Effects
  • Camera Amplification
  • Test signal 300 mV sine wave
  • Frequency 10-1050 Hz
  • Plot Amplification (Vcam/Vin) vs frequency
  • Frequency Dead Spots at 150 Hz multiples

10
Time Series Analysis Low Frequency
68 ms 15 Hz
Time Series Excerpt from Reduced Gravity
Parabola. Driving Frequency approximately 13 Hz.
The variation in frequency involves higher
harmonics
11
Time Series (high frequency)
2ms
High frequency analysis of time series shows
systematic peaks every 2ms. FFT should have peak
500 Hz.
12
Initial FFT Analysis
952 Hz
474.7 Hz
Series of harmonic peaks in high frequency (474.7
Hz fundamental) Insufficient resolution (1.5 Hz)
to distinguish low frequency response
13
Audio Parsing
  • Data Files split into 8 files each containing
    every 8th point
  • Sample rate decreases to 6 kHz (resolution
    improved to 0.25 Hz)
  • Parabola 19 driving frequency 17.5 Hz from motor
    data
  • Peaks in FFT show harmonics of 20 Hz
  • A few questions remain about the effectiveness/
    problems of parsing.

14
Modifications/Improvements for 2003 Flight
  • Sensors reconstructed and more solidly bonded to
    central plate of box set.
  • Sensor voltage amplified using standard inverting
    op-amp (impacts easier to detect)
  • Data collection controlled by a microcontroller
    and stored on a hard drive. (Sampling rate
    reduced to 2kHz)
  • Reliance on camera function for impact
    information avoided.
  • Coupling of signal eliminated

15
Impact Data Sample
16
Acknowledgements
  • Dr. Michael Wilson -- National Academy of
    Sciences
  • Mr. Shawn Jackson -- University of Tulsa
  • Rebecca Ragar, Jeffrey Wagner, Justin Eskridge,
    Adrienne McVey, Erin Lewallen, and Ian Zedalis.
  • Dr. Roger Blais -- University of Tulsa
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