Accession Number:

AD0701237

Title:

CALCULATIONS FOR STRENGTH AND OSCILLATIONS IN ROCKET ENGINES,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

• Gurov ,A. F.

Report Date:

1969-11-06

Pagination or Media Count:

492.0

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

Descriptors:

• (*LIQUID PROPELLANT ROCKET ENGINES
• ROCKET COMPONENTS)
• (*ROCKET COMPONENTS
• PERFORMANCE(ENGINEERING))
• TURBOPUMPS
• TURBINE BLADES
• TURBINE STATORS
• DRIVE SHAFTS
• FLEXIBLE SHAFTS
• OSCILLATION
• DAMPING
• RESONANCE
• MATHEMATICAL ANALYSIS
• USSR
• TEXTBOOKS

Subject Categories:

• Mechanics
• Liquid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE