Jet Engine Theory (Turbomachines) (Selected Chapters),

Abstract

This book is intended for students of the aviation institutes and may be useful for scientific personnel and engineers working in the gas turbine engine field. It presents theory, design methods, and flow passage component profiling techniques, and examines the characteristics of compressors and turbines used in turbojet and turboprop engines. The authors have also used the literature available on rotor, stator and jet engine theory.

Document Details

Document Type
Technical Report
Publication Date
Jan 22, 1975
Accession Number
ADA007175

Entities

People

  • B. S. Stechkin
  • P. K. Kazandzhan

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Human Systems

DTIC Thesaurus Topics

  • Engines
  • Gas Turbine Regenerators
  • Gas Turbines
  • Jet Engines
  • Scientists
  • Turbine Components
  • Turbines
  • Turbojet Engines
  • Turboprop Engines

Fields of Study

  • Engineering

Readers

  • Aerodynamics.
  • Aerospace Engineering
  • Library and Information Science