Accession Number : AD0786959
Title : Design and Strength of Aircraft and Helicopters,
Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Personal Author(s) : Mirtova,K. D. ; Chernenko,Zh. S.
Report Date : 18 SEP 1974
Pagination or Media Count : 679
Abstract : The manual sets forth the sequence of the design and construction of flight vehicles; it relates the conditions of their loading, the selection of shapes and structure diagrams; it examines the general questions of design, strength and operation of the basic parts of flight vehicles, their reliability, durability and effectiveness. The manual corresponds to a course program intended for the students of higher educational institutions.
Descriptors : *Aircraft, *Helicopters, Aerodynamic loading, Airframes, Wing body configurations, Helicopter rotors, Rotor blades(Rotary wings), Ailerons, Aerodynamics, Aircraft engines, Landing gear, Fuselages, Translations, USSR
Subject Categories : Helicopters
Distribution Statement : APPROVED FOR PUBLIC RELEASE