NASA-TM-78813

Wind-tunnel force and flow visualization data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from minus 4 deg to 60 deg

Note:

This document has not been validated by ESDU. It is provided to our users as a useful reference source.

Abstract:

Flow visualization and force data for a series of six bodies of revolution are presented without analysis. The data were obtained in the Langley Unitary Plan wind tunnel for angles of attack from -4 deg to 60 deg. The Reynolds number used for these tests was 6,600,000 per meter.

Author(s):
E.J. Landrum; C.D. Babb

Indexed under:

  • None

Details:

NASA-TM-78813
Format:
  • PDF (from scanned original)
Status:
  • Original, issued 01 Jan 1979
Previous Releases:
  • None available