Accession Number:

AD0756102

Title:

Conditions for the Existence of a Normal Shock Wave in the Elements of Axial Supersonic Compressor,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1973-02-05

Pagination or Media Count:

27.0

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

Subject Categories:

  • Hydraulic and Pneumatic Equipment
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE