NASA-TM-X-213

Investigation of the aerodynamic characteristics of a supersonic horizontal- attitude VTOL airplane model at Mach numbers of 1.57, 2.14, 2.54, and 2.87

Note:

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

Abstract:

Drag and static longitudinal and lateral stability characteristics of supersonic horizontal attitude VTOL aircraft model in wind tunnel

Author(s):
A.E. Franklin; R.M. Lust

Indexed under:

  • None

Details:

NASA-TM-X-213
Format:
  • PDF (from scanned original)
Status:
  • Original, issued 01 Jan 1960
Previous Releases:
  • None available