INCREASING NOZZLE THRUST BY FLOW ROTATION,
Abstract
An analysis was made of the thrust obtainable with a rotating gas stream. A formula was obtained for the overall thrust.
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 05, 1968
- Accession Number
- AD0679803
Entities
People
- I. N. Naumova
- Yu. D. Shmyglevskii
Organizations
- National Air and Space Intelligence Center