Accession Number:

AD0204392

Title:

Experimental Investigation of The Hemisphere-Cylinder At Hypervelocities In Air

Descriptive Note:

Corporate Author:

ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN

Personal Author(s):

Report Date:

1958-11-01

Pagination or Media Count:

57.0

Abstract:

Pressure, heat transfer, drag, and shock detachment data were obtained for a hemisphere-cylinder model in the GDF Hotshot I hypervelocity wind tunnel.

Subject Categories:

  • Theoretical Mathematics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE