Publication Date:
2016-06-07
Description:
A method of obtaining test data from two independent models or bodies in a conventional wind tunnel is described. The system makes efficient use of wind tunnel test time with computer control performing complex coordinate transformations necessary for model positioning. The apparatus is designed to be used in any of the three Unitary Wind Tunnels at NASA-Ames Research Center. Mechanical design details and a brief description of the control system for the separation apparatus are presented.
Keywords:
MECHANICAL ENGINEERING
Type:
The 12th Aerospace Mech. Symp.; p 131-141
Format:
application/pdf