Accession Number:

ADA316543

Title:

Aerodynamic Dissemination.

Descriptive Note:

Final rept. 15 Jul 94-14 Jul 96,

Corporate Author:

MINNESOTA UNIV MINNEAPOLIS DEPT OF AEROSPACE ENGINEERING AND MECHANICS

Report Date:

1996-09-30

Pagination or Media Count:

14.0

Abstract:

We have built a shock tube and liquid injection system for studying the aerodynamic breakup of thickened TEP and other viscoelastic liquids under conditions that simulate high altitude, high Mach number intercept conditions.

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE