DETERMINING PERMISSIBLE IMBALANCES FOR THE ROTORS OF AVIATION GAS TURBINE ENGINES (OPREDELENIYE DOPUSTIMOY NEURAVNOVESHENNOSTI ROTOROV AVIATSIONNYKH GTD),
Abstract
A brief review of previous research is given. A general discussion is presented concerning the establishment of tolerances in the design of gas turbines.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1968
- Accession Number
- AD0831451
Entities
People
- A. A. Chistyakov