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NASA Technical Note [NASA TN D-3029]: Semiempirical method for predicting effects of incident-reflecting shocks on the turbulent boundary layer

By: Washington. National Aeronautics and Space Administration (NASA).
Contributor(s): Pinckney, S. Z.
Material type: materialTypeLabelBookSeries: National Aeronautics and Space Administration ; NASA Technical Note. Publisher: Washington NASA 1965Description: 99p.Subject(s): Aircraft | Hypersonic airbreathing propulsion systems | Turbulent boundary layer
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