Methods for determining the equivalent aerodynamic damping of reentry vehicle models tested in a setup with free oscillations

Author:

Chasovnikov E. A.,Chasovnikov S. A.

Publisher

Pleiades Publishing Ltd

Subject

Nuclear and High Energy Physics,Radiation

Reference6 articles.

1. Yu. M. Lipnitskii, A. V. Krasilnikov, A. N. Pokrovskil, and V. N. Shmanenkov, Unsteady Aerodynamics of Ballistic Flight, Fizmatlit, Moscow, 2003.

2. C. D. Kazemba, R. D. Braun, L. G. Clark, and M. Schoenenberger, Survey of blunt body dynamic stability in supersonic flow, AIAA Paper No. 2012-4509, 2012, P. 1–27.

3. N. P. Adamov, A. M. Kharitonov, E. A. Chasovnikov, A. A. Dyad’kin, A. N. Krylov, and E. N. Aleksandrov, Experimental study of aerodynamic characteristics of a reentry vehicle on a setup with free oscillations at supersonic velocities, Thermophysics and Aeromechanics, 2016, Vol. 23, No. 6, P. 791–800.

4. N. M. Krylov and N. N. Bogolyubov, Introduction into Nonlinear Mechanics, AN USSR, Kiev, 1937.

5. B. Redd, D. M. Olsen, and R. L. Barton, Relationship between the aerodynamic damping derivatives measured as a function of instantaneous angular displacement and the aerodynamic derivatives measured as a function of oscillation amplitude, NASA-TN-D-2855, 1965.

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