FORMATION OF THE FLOW PATH OF A TURBINE BY UNDERCUTTING BLADES OF THE INITIAL STAGE

Abstract

The analysis shows that at the present time it is advisable to form and calculate the flow paths of turbines by the method of model stages. This method specifies the formation of the flow path from initial stage by undercutting the blades for the given operating conditions of a group of stages, and in certain cases, of the entire flow path of an individual turbine cylinder or of the turbine as a whole.

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Document Details

Document Type
Technical Report
Publication Date
Feb 19, 1962
Accession Number
AD0273406

Entities

People

  • A.m. Zavadovskiy
  • Kh.l. Babenko

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Boundaries
  • Department Of Defense
  • Diameters
  • Efficiency
  • Engineers
  • Gas Turbines
  • Government Procurement
  • Governments
  • Guide Vanes
  • Procurement
  • Reactivities
  • Resistance
  • Rotation
  • Translations
  • Turbines

Readers

  • Aerodynamics.
  • Fluid Dynamics.
  • Systems Analysis and Design