WIND TUNNEL,
Abstract
A wind tunnel has been designed for the purpose of investigating boundary layer in a semirestricted stream under conditions of gradientless and gradient flow at greater flow velocities and constant pressure over a length of ten calibers of pressure nozzle. The working section is made in form of a rectangular trough with solid bottom and side walls and free flexible upper wall. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 16, 1963
- Accession Number
- AD0420660
Entities
People
- A. M. Mkhitaryan
- V.s. Maksimov
Organizations
- National Air and Space Intelligence Center