Accession Number:

AD0612618

Title:

STRUCTURAL MECHANICS OF THE AIRPLANE,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

• UMANSKII,A. A.

Report Date:

1965-03-15

Pagination or Media Count:

676.0

Abstract:

The volume is a study aid for the aviation high schools on the subject Structural Mechanics of the Airplane which contains the fundamental theoretical basis for the static calculations set forth in the course strength calculations for the airplane. The book sets forth the problems of complex beam bending, strength and stability of plates and shells, strength and bearingability calculations for structures of the wing and fuselage type, calculations for flat and three-dimensional girders, and a number of auxiliary problems with the appropriate mathematical apparatus. The book reflects the contemporary level of theoretical knowledge in the field of the structural mechanics of aviation structures, and may be employed by engineers in the industry in their practical work. Author

Descriptors:

• *AIRCRAFT
• *AIRFRAMES
• STRUCTURAL COMPONENTS
• FUSELAGES
• WINGS
• HORIZONTAL STABILIZERS
• STRUCTURES
• SHELLS(STRUCTURAL FORMS)
• FLANGES
• LOADS(FORCES)
• STABILITY
• MATHEMATICAL ANALYSIS
• USSR

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE