Showing 1 - 19 results of 19 for search 'Wisnoe, W.', query time: 0.12s Refine Results
  1. 1
    Thermal Uniformity Study in a Circular Divergent Diffuser with Swirl Flow Generator
    by Shukri, ES, Wisnoe, W
    Published 2019
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  2. 2
    Wavelet transform of acoustic signal from a Ranque-Hilsch Vortex Tube
    by Istihat, Y., Wisnoe, W.
    Published 2015
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    Article
  3. 3
    Wavelet Transform Of Acoustic Signal From A Ranque-Hilsch Vortex Tube
    by IOP, Istihat, Y, Wisnoe, W
    Published 2015
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    Article
  4. 4
    Thermal uniformity study in a circular divergent diffuser with swirl flow generator
    by Bevrani H., Shukri, E.S, Wisnoe, W.
    Published 2019
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    Article
  5. 5
    Aerodynamic, stability and flying quality evaluation on a small blended wing-body aircraft with canard foreplanes
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    Article
  6. 6
    Thermofluid-Acoustic Analysis of a Ranque-Hilsch Vortex Tube
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    Article
  7. 7
    The Effect of Orifice Diameter to the Acoustic Signals Captured at the Cold Part of a Ranque-Hilsch Vortex Tube
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    Article
  8. 8
    The study of water media in Green Tower's solar collector
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  9. 9
    Aerodynamic Analysis of Blended Wing Body - Unmanned Aerial Vehicle (BWB-UAV) Equipped with Horizontal Stabilizers
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  10. 10
    A blended wing body airplane with a close-coupled, tilting tail
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  11. 11
    An analysis on 45 degrees sweep tail angle for blended wing body aircraft to the aerodynamics coefficients by wind tunnel experiment
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  12. 12
    A blended wing body airplane with a close-coupled, tilting tail
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  13. 13
    Aerodynamic characteristics of a cranked planform blended wing-body aircraft with 40° sweep angle
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  14. 14
    Aerodynamics analysis on the effect of canard aspect ratio on blended wing body aircraft using CFD simulation
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  15. 15
    Aerodynamic characteristics of a cranked planform blended wing-body aircraft with 40° sweep angle
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  16. 16
    An analysis on 45° sweep tail angle for blended wing body aircraft to the aerodynamics coefficients by wind tunnel experiment
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    Article
  17. 17
    Aerodynamics of a blended wing body aircraft with close-coupled tail: Computational Fluid Dynamics simulations of two different tail sweep angle cases
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  18. 18
    The Effect of Orifice Diameter to the Acoustic Signals Captured at the Cold Part of a Ranque-Hilsch Vortex Tube
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  19. 19
    Comparison on the aerodynamic coefficients obtained from three different size of wind tunnel model on Baseline V set at 45 degree sweep tail angle
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