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Accession Number:
AD0622400
Title:
The External Loads and Strength of Flying Apparatuses
Descriptive Note:
[Technical Report, Monograph]
Corporate Author:
AIR FORCE SYSTEMS COMMAND WRIGHT-PATTERSON AFB OH
Report Date:
1965-07-20
Pagination or Media Count:
633
Abstract:
This book is dedicated to external loads having effect on a flight vehicle aircraft and helicopter, and the durability of its construction. Basic attention in the book is allotted to actual problems of strength of contemporary flight vehicles dynamic load, periods of service and strength of construction, strength during high speeds of flight, taking into account aerodynamic heating and others. Along with an account of theoretical questions in the book there are described experimental methods of investigating strength of construction. The book is designed for engineers connected with designing, tests, and exploitation of flight vehicles. At the same time, it can be used as a training aid for aviation students of higher educational institutions.
Distribution Statement:
[A, Approved For Public Release]
