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Investigation of the effect of parameter mistuning on the strength characteristics of turbine elements
Repetckii O.V., Nguyen V.
Parametric analysis of the anisogrid body of the spacecraft for cleaning the orbit of space debris
Belonovskaya I.D., Kolga V.V., Yarkov I.S., Yarkova E.A.
EXPERIMENTAL AND THEORETICAL GROUND-BASED TESTING OF SPACECRAFT ANTENNAS
Dvimiy G.V., Eresko S.P.
Algorithm for simulation of vibration effects during track tests of aircraft and missile technology
Astakhov S.A., Biryukov V.I., Borovikov D.A.
DETERMINATION OFTHE FUNDAMENTAL FREQUENCY FOR RECTANGULARSANDWICH PLATE WITH TWO FREE EDGES
Lopatin A.V., Deev P.O., Lopatin A.V., Deev P.O.
DETERMINATION OF FUNDAMENTAL OSCILLATION FREQUENCY OF THE RECTANGULAR SANDWICH PLATE TIGHTENED IN THE CENTRAL POINT
Deev P.O.
Determination of the fundamental frequency for rectangular sandwichplate with free edge
Lopatin A.V., Deev P.O.
DETERMINATION OF THE FUNDAMENTAL FREQUENCY OF A SANDWICH PANEL AS CONSTRUCTIONAL PART OF SPACECRAFT BODY
Deev P.O., Sinkovskiy F.K.
DETERMINATION OF VIBRATIONS DOMINANT MODE OF AN ORTHOTROPIC PLATE FASTENED TO THE BEDDING ANGLES
Lopatin I.A.
FUNDAMENTAL FREQUENCY DETERMINATION FOR SANDWICH PLATE SIMPLY SUPPORTED IN FOUR CORNERS
Deev P.O., Lopatin A.V.
1 - 10 of 10 Items

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