Aviation Engine Vibration Theory and Calculation
Abstract
The book deals with basic data on the general theory of vibrations of linear and nonlinear systems, their application to calculation of vibrations of parts, units and systems of aircraft engines. Given are contemporary methods for calculation of vibrations, which are developing in connection with the use of high speed computers; the method of initial parameters, the method of dynamic rigidities, the methods of discrete models and the integral method. The book represents a text book for students specializing in the strength of aircraft engines; it can be useful also to engineers of the aircraft industry.
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 01, 1971
- Accession Number
- AD0731351
Entities
People
- D. V. Khronin
Organizations
- National Air and Space Intelligence Center