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)
Structural Mechanics of the Airplane
1965
2 pages
Report
No indication
English
AIRPLANES , AIRFRAMES , STRUCTURAL PARTS , MECHANICAL PROPERTIES , FUSELAGES , WINGS , AERIAL RUDDERS , STABILIZERS (HORIZONTAL TAIL SURFACE) , BEAMS (STRUCTURAL) , STRUCTURES , REINFORCING MATERIALS , STRUCTURAL SHELLS , FLANGES , CYLINDRICAL BODIES , DESIGN , LOADING (MECHANICS) , STABILITY , METAL PLATES , MATHEMATICAL ANALYSIS , USSR , Translations
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