Accession Number:

AD0631649

Title:

EXPERIMENTAL INVESTIGATION OF THE SURFACE IMPACT PRESSURE PROBE METHOD OF MEASURING LOCAL SKIN FRICTION AT SUPERSONIC SPEEDS.

Descriptive Note:

Master's thesis,

Corporate Author:

DEFENSE RESEARCH LAB UNIV OF TEXAS AUSTIN

Personal Author(s):

Report Date:

1958-01-01

Pagination or Media Count:

124.0

Abstract:

The purpose of the report is to demonstrate, on the basis of wind tunnel results, the feasibility of using a surface probe. This phase is limited to thermally insulated surfaces with zero pressure gradient.

Subject Categories:

  • Test Facilities, Equipment and Methods
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE