SELECTION OF THE OPTIMAL DEGREE OF REACTION OF THE STAGES OF A GAS TURBINE WITH UNSHROUDED BLADES.

Abstract

There are presented the results of computational investigations for determining the optimal degree of reaction for the stages of gas turbines with unshrouded guiding and operating blades. The work was carried out on the electronic computer Ural-l. The results are compared with the experimental data. (Author)

Document Details

Document Type
Technical Report
Publication Date
Apr 08, 1966
Accession Number
AD0637386

Entities

People

  • G. V. Prokuryakov

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Computers
  • Experimental Data
  • Gas Turbines
  • Turbines

Fields of Study

  • Chemistry
  • Physics

Readers

  • Aerodynamics.
  • Molecular Photonics/Laser Physics
  • Systems Analysis and Design

Technology Areas

  • Microelectronics