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Figure 11-3. Comparison of the modified Newtonian estimate over the nose of a blunted cone with wind tunnel data (Model 2 in TN D-4865).[1]

Figure 11-3. Comparison of the modified Newtonian estimate over the nose of a blunted cone with wind tunnel data (Model 2 in TN D-4865).[footnote]Charlie M. Jackson, Jr., and Wallace C. Sawyer, “A Method for Determining Surface Pressures on Blunt Bodies of Revolution at Small Angles of Attack in Supersonic Flow,” NASA TN D- 4865, 1968 Note this report includes results from a wind tunnel test, and has the tab data.[/footnote]
  1. Charlie M. Jackson, Jr., and Wallace C. Sawyer, “A Method for Determining Surface Pressures on Blunt Bodies of Revolution at Small Angles of Attack in Supersonic Flow,” NASA TN D- 4865, 1968 Note this report includes results from a wind tunnel test, and has the tab data. ↵

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