EXPERIMENTS ON IMPACT PRESSURE PROBES IN A RAREFIED SUBSONIC GAS STREAM,
Abstract
The performance of impact pressure probes (having a length to internal diameter ratio of about 10) in a rarefied subsonic gas stream was studied. The range of Knudsen numbers (based on internal diameter of the probe) was 1.0 to 15.0 and the range of the speed ratios 0.1 to 0.6. All experiments were conducted in a low density gas dynamics facility using nitrogen as the test gas. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1967
- Accession Number
- AD0661384
Entities
People
- A. K. Sreekanth
Organizations
- Boeing