| Nikolay
I. Baranov, Pavel D. Nushtaev, Yury P. Nushtaev |
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| Control
Surface Flutter of Aircraft and Rockets. |
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This books gives an account of a number of
research methods and practical measures to prevent the flutter of
control surfaces on aircraft and winged rockets in the USSR during
the 1950's 1980's.
The book consists of three parts.
Part one shows facts and figures regarding accidents that occurred
during flight-tests, caused by flutter of control surfaces as well
rational means to prevent this dangerous phenomenon.
In the second part, research methods to establish different modes
of flutter are presented whereby the individual mode of vibration
is directly linked to the aerodynamic characteristics of the
aircraft and rocket in question.
The third part of the book focuses on theoretical research and
experimental studies of control surfaces non-steady aerodynamic
data at the different states of flight, especially at the
transonic Mach
range.
The book is intended for aviation specialists, designers and
constructors engaged in the building
and testing of aircraft and rockets. |
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