NASA-CR-61365

Results of a study of Mach number and Reynolds number effects on the crossflow drag characteristics of ogive cylinders and ogive-cylinder-frustum-cylinders at angles of attack to 30 degrees

Note:

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

Abstract:

An analysis was made to determine the effects of Mach number and Reynolds number on the local and total crossflow drag characteristics of ogive-cylinders and ogive-cylinder-frustum-cylinders at angles of the MSFC 14 in TWT and the LTV 4 ft HSWT, and pressure data obtained in the TWT, at Mach numbers 0.14, 0.8, 1.2, and 2.0, and a wide range of Reynolds numbers. Results indicate that the streamwise Reynolds number, VD/nusin alpha, is an important correlation parameter in the subcritical Reynolds number range at imcompressible speeds and that the crossflow Mach number correlates compressibility effects.

Author(s):
J.E. Foley

Indexed under:

  • None

Details:

NASA-CR-61365
Format:
  • PDF (from scanned original)
Status:
  • Original, issued 01 Jan 1971
Previous Releases:
  • None available