Accession Number : AD0696042

Title :   STRUCTURE AND STRENGTH OF AIRCRAFT GAS-TURBINE ENGINES,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Pallei,Z. S. ; Korolev,I. M. ; Rovinskii,E. V.

Report Date : 14 MAY 1969

Pagination or Media Count : 415

Abstract : This book is intended for mechanical engineering students intending to work in civil aviation. The book deals with the principal structural members and systems of aircraft gas-turbine engines and with their advantages and short-comings. Strength and vibration calculation methods are presented along with data on critical rotor speeds. (Author)

Descriptors :   (*GAS TURBINES, TEXTBOOKS), TURBOJET ENGINES, TURBOPROP ENGINES, TURBOJET INLETS, ICE PREVENTION, GAS TURBINE ROTORS, GAS TURBINE BLADES, STRUCTURAL PROPERTIES, MECHANICAL PROPERTIES, COMBUSTION CHAMBERS, GAS TURBINE NOZZLES, REDUCTION GEARS, LUBRICATION, EXHAUST SYSTEMS, USSR

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE