CALCULATIONS FOR STRENGTH AND OSCILLATIONS IN ROCKET ENGINES,

Abstract

In the book are expounded methods of calculation for strength and oscillations of components and subassemblies of rocket engines. In particular, there are considered strength and oscillations of turbine blades of turbopump unit, strength of turbopump unit turbine disks, allowable stresses and safety factors for these elements of the engine. Calculations are listed on the strength of housing shells of engine and combustion chambers. There are examined associated oscillations of various complex systems, critical speed of rotation of shafts damping of oscillations and shock absorption. (Author)

Document Details

Document Type
Technical Report
Publication Date
Nov 06, 1969
Accession Number
AD0701237

Entities

People

  • A. F. Gurov

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Chambers
  • Combustion
  • Combustion Chambers
  • Complex Systems
  • Engines
  • Oscillation
  • Rocket Engines
  • Rockets
  • Safety Factor
  • Turbine Blades
  • Turbines
  • Turbopumps

Readers

  • Aerodynamics.
  • Software Engineering
  • Structural Dynamics.