Study of Self-Excited Pitch Oscillations of Conical-Spherical Body at Mach Number M = 1.75 and Two Moments of Inertia
https://doi.org/10.25205/2541-9447-2023-18-1-43-52
Abstract
Tests of a conical-spherical body in a supersonic wind tunnel were carried out on a free oscillation installation along the pitch angle at a Mach number M = 1.75 and two moments of inertia of the body relative to the axis of rotation. For a body with a large moment of inertia, self-oscillations with the amplitude of ca. 10 deg were obtained. For the first time, the phenomenon of degeneration of self-oscillations for a body with a smaller moment of inertia has been discovered. An attempt was made to model the phenomenon using an ordinary linear differential equation of the first order
About the Authors
N. A. MishchenkoRussian Federation
Nikita A. Mishchenko, Laboratory Assistant, Khristianovich Institute of Theoretical and Applied
Mechanics SB RAS
Novosibirsk
E. A. Chasovnikov
Russian Federation
Evgeniy A. Chasovnikov, Candidate of Engineering Sciences, Senior Researcher, Khristianovich Institute of Theoretical and Applied Mechanics SB RAS
References
1. Kazemba C. D., Braun R. D., Clark L. G., Schoenenberger M. Survey of Blunt Body Supersonic Dynamic Stability // Journal of Spacecraft and Rockets. Vol. 54, no. 1. 2017. P. 109–127.
2. Adamov N. P., Chasovnikov E. A. Self-induced oscillations of a cone with a hemispherical rear part at low supersonic velocities // American Institute of Physics Conference Proceedings, 2018. Vol. 2027. P. 030150-1–030150-5.
3. Fedyaevsky K. K., Blyumina L. Kh. Hydrodynamics of separated flow. M.: Mashinostroenie, 1977. 120 p.
4. Chasovnikov E. A., Chasovnikov S. A. On similarity criteria at the experimental modeling of the flying vehicles motion with the aid of small-scale models // Thermophysics and Aeromechanics. 2017. Vol. 24, no. 1. P. 1–6.
5. Chasovnikov E. A., Chasovnikov S. A. Methods for determining the equivalent aerodynamic damping of reentry vehicle models tested in a setup with free oscillations // Thermophysics and Aeromechanics. 2019. Vol 26, no. 1. P. 1–8.
6. Chasovnikov E. A. Specific features of the aerodynamic moment and the pitch damping of a re-entry vehicle model exercising free oscillations at supersonic speeds // Thermophysics and Aeromechanics. 2020. Vol. 27, no. 3. P. 331–338.
7. Chasovnikov E. A. Mathematical modeling of self-induced oscillations of a segmental-conical body with free movement in the pitch angle / American Institute of Physics Conference Proceedings, 2021. P. 030073-1–030073-22. DOI 10.1063/5.0051976
8. Adamov N. P., Gurin A. M., Chasovnikov E. A. Methodical investigations of aerodynamic derivatives of a sharp cone on a setup with free oscillations at supersonic velocities / American Institute of Physics Conference Proceedings. 2018. Vol. 2027. P. 030151-1–030151-8.
9. Belotserkovsky S. M., Skripach B. K., Tabachnikov V. G. Wing in non-stationary gas flow. M.: Nauka, 1971. 768 p.
10. Adamov N. P., Mishchenko N. A., Chasovnikov E. A. About the Dynamic Damping Coefficients of a Segmental-Cone Model at Mach M = 2.3 // Siberian Journal of Physics. 2022. Vol. 17, no. 1. P. 34–46.
11. Abe T., Sato S., Matsukawa Y., Yamamoto K., Hiraoka K. Study for dynamically unstable motion of reentry capsule. The institute of Space and Astronautical science // Report SP No. 17, 2003. P. 301–332.
12. Chasovnikov E. A. On the issue of separating complexes of aerodynamic derivatives for problems of aircraft flight dynamics // Izvestiya vuzov. Aviation technology. 2011. No. 3. P. 47–49.
13. Tobak M., Wehrend W. R. Stability derivetives of cones at supersonic speeds // NASA AMES, 1956. Technical Note № 3788. 43 p.
Review
For citations:
Mishchenko N.A., Chasovnikov E.A. Study of Self-Excited Pitch Oscillations of Conical-Spherical Body at Mach Number M = 1.75 and Two Moments of Inertia. SIBERIAN JOURNAL OF PHYSICS. 2023;18(1):43-52. (In Russ.) https://doi.org/10.25205/2541-9447-2023-18-1-43-52