Pressure distribution and some effects of viscosity on slender inclined bodies of revolution /
H. Julian Allen.

Description

Main Author

Allen, H. Julian.

Related Names

United States. National Advisory Committee for Aeronautics.

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, 1950.

Subjects

Body of revolution.
Viscous flow.
Aerodynamic load.

Summary

The simplified solution for the pressure distribution of slender inclined bodies of revolution is developed. The solution should be suitable for bodies of high fineness ratio even at low supersonic speeds, provided the angle of attack is small. Comparison with low-speed experimental results indicates that the observed flow separation phenomena can be explained in terms of the calculated pressure distributions together with the theory of oblique viscous flows.

Note

NACA TN No. 2044.
"March 1950."

Physical Description

19 p. : ill. ; 28 cm.

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