ENGINEERING CALCULATIONS FOR GAS TURBINE ENGINES BY THE METHODS OF SMALL DEVIATIONS,

Abstract

This book is intended for engineers engaged in the research, development, and designing of stationary and aviation gas-turbine engines and it may also be useful to professors and student in schools of higher education. A simple method is presented of calculating the interdependence of the working process parameters of all contemporary types of gas-turbine engine arrangements, i.e., turbojet, engines with two-stage compressors, and so forth. The effect of variations in parameters or the chracteristics of engine components, e.g., coefficient of losses, efficiency, etc., on thrust, power, air intake, and fuel are calculated by the method of small deviations and converted into a system of linear algebraic equations, which yield both general and specific answers to practical problems. Examples illustrating the use of the method are given and the limitations of the method as well as its margin of error are also covered. (Author)

Document Details

Document Type
Technical Report
Publication Date
Feb 03, 1969
Accession Number
AD0692495

Entities

People

  • A. Ya. Cherkez

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Air Intakes
  • Engine Components
  • Engine Fuel Systems Components
  • Engineering
  • Engineers
  • Engines
  • Gas Turbines
  • Linear Algebraic Equations
  • Turbine Components
  • Turbines
  • Turbojet Engines

Fields of Study

  • Engineering

Readers

  • Combustion and Flow Dynamics.
  • Regression Analysis.
  • Systems Analysis and Design