Accession Number:

AD0744183

Title:

Theory and Design of Aircraft Turbomachines,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

• Kholshchevnikov,K. V.

Report Date:

1972-02-29

Pagination or Media Count:

980.0

Abstract:

The textbook examines the fundamentals of turbomachine theory and also the configurations and operating principles of turbomachines of various types - axial, centrifugal, and mixed-flow compressors and axial turbines. Considerable attention is devoted to turbine and compressor performance and regulation and also the problems of matching their parameters in the gas turbine engine system. The text is intended for students of aviation colleges and schools. It may also be used by engineering and technical personnel working in aircraft engine construction. Author

Descriptors:

• CENTRIFUGAL COMPRESSORS
• COMPRESSOR COMPONENTS
• TURBINE COMPONENTS
• USSR

Subject Categories:

• Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE