Transonic Flow at a Slotted Test Section Wall.
Abstract
A brief preview is given of some important features of slot flow as they are beginning to emerge from the present experimental and theoretical investigation. It is tentatively concluded, for a particular case typical of two-dimensional tests, that the slot flow is approximately inviscid (although influenced by boundary layer formation in the slot), that it leaves the slot as a free jet, that it is influenced by the test section wall boundary layer, and that the quadratic cross flow term in the pressure difference formula is important. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 01, 1974
- Accession Number
- AD0784934
Entities
People
- Hans Sorensen
- Sune B. Berndt
Organizations
- National Aeronautical Research Institute