Document Details

Transonic Wind Tunnel Tests of a Model of the Sandia Sauterne Shape-- Phase III
Reid, C F [Cornell Aeronautical Laboratory, Inc.-- Sandia Contract Purchase Order 4804-009]
Document Type:
Publication Date:
1965 Mar 01
Document Pages:
233 p.
Document Number(s):
SC-DC-65-1531X; ALSNL199700001499
Originating Research Org.:
Sandia National Lab. (SNL-NM), Albuquerque, NM (United States)
OpenNet Entry Date:
1999 Sep 28
OpenNet Modified Date:
1999 Sep 28
These tests were performed in order to determine longitudinal and lateral static stability characteristics of the model with several tailfin configurations. The tests were performed at Mach numbers from 0.6 to 1.2 at various angles of attack.

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