naa a22 4500 510758495 CHVBK 20180411083130.0 cr unu---uuuuu 180411e20131201xx s 000 0 eng 10.1134/S0869864313060103 doi (NATIONALLICENCE)springer-10.1134/S0869864313060103 Aerodynamic derivatives of the model of the jettisonable module of the emergency rescue system at hypersonic velocities [Elektronische Daten] [N. Adamov, L. Puzyrev, A. Kharitonov, E. Chasovnikov, A. Dyadkin, A. Krylov] The model, experimental equipment, and test program are briefly described. A method of determining the aerodynamic characteristics of the model on the facility with free oscillations is presented. Aerodynamic derivatives of the pitching moment of the model are obtained for two positions of the axis of rotation and Mach numbers M∞ = 2, 4, and 6. At M∞ = 2, the model with the rear position of the axis of rotation is not balanced at low angles of attack, whereas irregular self-sustained oscillations of the model with the frontal position of the axis of rotation arise. Pleiades Publishing, Ltd., 2013 jettisonable module model nationallicence free oscillations nationallicence oscillation frequency nationallicence damping decrement nationallicence aerodynamic derivatives nationallicence Adamov N. Khristianovich Institute of Theoretical and Applied Mechanics SB RAS, Novosibirsk, Russia aut Puzyrev L. Khristianovich Institute of Theoretical and Applied Mechanics SB RAS, Novosibirsk, Russia aut Kharitonov A. Khristianovich Institute of Theoretical and Applied Mechanics SB RAS, Novosibirsk, Russia aut Chasovnikov E. Khristianovich Institute of Theoretical and Applied Mechanics SB RAS, Novosibirsk, Russia aut Dyadkin A. Korolev Rocket and Space Corporation "Energia”, Korolev, Moscow Region, Russia aut Krylov A. Korolev Rocket and Space Corporation "Energia”, Korolev, Moscow Region, Russia aut Thermophysics and Aeromechanics Kutateladze Institute of Thermophysics SB RAS 20/6(2013-12-01), 729-738 0869-8643 20:6<729 2013 20 11510 https://doi.org/10.1134/S0869864313060103 text/html Onlinezugriff via DOI 1 research-article jats NATIONALLICENCE 856 40 https://doi.org/10.1134/S0869864313060103 text/html Onlinezugriff via DOI NATIONALLICENCE 700 1- Adamov N. Khristianovich Institute of Theoretical and Applied Mechanics SB RAS, Novosibirsk, Russia aut NATIONALLICENCE 700 1- Puzyrev L. Khristianovich Institute of Theoretical and Applied Mechanics SB RAS, Novosibirsk, Russia aut NATIONALLICENCE 700 1- Kharitonov A. Khristianovich Institute of Theoretical and Applied Mechanics SB RAS, Novosibirsk, Russia aut NATIONALLICENCE 700 1- Chasovnikov E. Khristianovich Institute of Theoretical and Applied Mechanics SB RAS, Novosibirsk, Russia aut NATIONALLICENCE 700 1- Dyadkin A. Korolev Rocket and Space Corporation "Energia”, Korolev, Moscow Region, Russia aut NATIONALLICENCE 700 1- Krylov A. Korolev Rocket and Space Corporation "Energia”, Korolev, Moscow Region, Russia aut NATIONALLICENCE 773 0- Thermophysics and Aeromechanics Kutateladze Institute of Thermophysics SB RAS 20/6(2013-12-01), 729-738 0869-8643 20:6<729 2013 20 11510 Metadata rights reserved Springer special CC-BY-NC licence nationallicence BK010053 XK010053 XK010000 NATIONALLICENCE NATIONALLICENCE NL-springer