NACA-TN-4347
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- March 24, 2016 Create Date
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National Advisory Committee for Aeronautics, Technical Notes - A Nonlinear Theory for Predicting the Effects of Unsteady Laminar, Turbulent, or Transitional Boundary Layers on the Attenuation of Shock Waves in a Shock Tube with Experimental Comparison
| File | Action |
|---|---|
| naca-tn-4347 A Nonlinear Theory for Predicting the Effects of Unsteady Laminar, Turbulent, or Transitional Boundary Layers on the Attenuation of Shock Waves in a Shock Tube with Experimental .pdf | Download |
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