Conditions for the Existence of a Normal Shock Wave in the Elements of Axial Supersonic Compressor,
Abstract
Due to the rise of velocities in the running section of a compressor, of ever increasing interest is the problem dealing with stagnation of supersonic swirling flows in shock waves. In this work, conditions are found for the existence of a normal shock wave in the interblade channels of a rotor and the stator of the axial supersonic stage with a finite number of blades, and equations which permit one to calculate flows satisfying these conditions are given. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 05, 1973
- Accession Number
- AD0756102
Entities
People
- G. A. Freyman
- Yu. N. Vasilev
Organizations
- National Air and Space Intelligence Center