Simplified Method for the Prediction of Aerofoil Excrescence Drag Magnification Factor for Turbulent Boundary Layers at Subcritical Mach Numbers. 91028

Simplified Method for the Prediction of Aerofoil Excrescence Drag Magnification Factor for Turbulent Boundary Layers at Subcritical Mach Numbers. 91028

  • Loose-leaf

Currently unavailable

We can notify you when this item is back in stock

Add to wishlist

AbeBooks may have this title (opens in new window).

Try AbeBooks

Product details

  • Loose-leaf
  • London, United Kingdom
  • 0856797901
  • 9780856797903