A SUPERSONIC AXISYMMETRICAL NOZZLE FOR WIND TUNNELS,
Abstract
For the purpose of lowering the thermal stresses and temperature deformations which distort the configuration of the flow part the uncooled nozzle is designed in bracket fashion.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 29, 1965
- Accession Number
- AD0620074
Entities
People
- Alexander S. Sokolov
- L. N. Kopp
Organizations
- National Air and Space Intelligence Center