EXPERIMENTAL INVESTIGATION OF THE SURFACE IMPACT PRESSURE PROBE METHOD OF MEASURING LOCAL SKIN FRICTION AT SUPERSONIC SPEEDS.
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.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1958
- Accession Number
- AD0631649
Entities
People
- Charles Joe Stalmach Jr.