[1] J.H. Allen, Motion of a ballistic missile angularly misaligned with the flight path upon entering the atmosphere and its effect upon aerodynamic heating,aerodynamic loads, and miss distance, NACA TN4048,(1957).
[2] T. Babineaux, J. Brayshaw Jr, B. Dayman Jr, D. Nelson,The influence of shape on aerodynamic damping of oscillatory motion during planet atmosphere entry and measurement of pitch damping at large oscillation amplitudes, NACA TR32-380, (1963).
[3] J.D. Bird, D.E. Reese Jr, Stability of ballistic reentry bodies, NACA RM L58E02A, (1958).
[4] G.T. Chapman, C. Berner, W.H. Hathaway, G.Winchenbach, R. Mitcheltree, The use of spherical bases to eliminate limit cycles of blunt entry vehicles, AIAA Paper, 1023 (1999) 1999.
[5] H. Fletcher, W. Wolhart, Damping in pitch and static stability of supersonic impact nose cones, and manned reentry capsules at mach numbers from 1.93 to 3.05,NASA TM X-347, (1960).
[6] C.H. Whitlock, P.M. Siemers, Parameters influencing dynamic stability characteristics of Viking-type entry configurations at mach 1.76, Journal of Spacecraft and Rockets, 9(7) (1972) 558-560.
[7] P. Jaffe, Dynamic stability tests of spinning entry bodies in the terminal regime, Journal of Spacecraft and Rockets, 8(6) (1971) 575-579.
[8] M.V. Krumins, Drag and Stability of Mars Probe/Lander Shapes, Journal of Spacecraft and Rockets, 4(8) (1967)1052-1057.
[9] F.D. Steketee, Dynamic stability of space vehicles, NACACR-935 (1967).
[10] A. Guidi, Q. Chu, J. Mulder, F. Nicolosi, Virtual reality modeling simulation of the re-entry motion of an axialsymmetric vehicle, in: 34th COSPAR Scientific Assembly, TX USA, 2002.
[11] D.B. Owens, V.V. Aubuchon, Overview of orion crew module and launch abort vehicle dynamic stability, in:29th AIAA Applied Aerodynamics Conference, Hawaii,USA, 2011.
[12] S. Koga, A. Hidaka, R. Tagai, T. Kimura, T. Yoshinaga,S. Nagai, H. Nishijima, Dynamic stability testing of a reentry lifting capsule in a transonic wind tunnel, in: 52nd Aerospace Sciences Meeting, Maryland, USA,2014.
[13] S.M. Murman, Dynamic simulations of atmosphericentry capsules, Journal of Spacecraft and Rockets, 46(4)(2009) 829-835.
[14] E. Stern, V. Gidzak, G.V. Candler, Estimation of dynamic stability coefficients for aerodynamic decelerators using CFD, in: AIAA Applied Aerodynamics Conference, New Orleans, LA, 2012.
[15] S. Teramoto, K. Hiraki, K. Fujii, Numerical analysis of dynamic stability of a reentry capsule at transonic speeds,AIAA journal, 39(4) (2001) 646-653.
[16] S. Teramoto, K. Fujii, Mechanism of dynamic instability of a reentry capsule at transonic speeds, AIAA journal,40(12) (2002) 2467-2475.
[17] T. Abe, S.i. Sato, Y. Matsukawa, K. Yamamoto, K.Hiraoka, Study for dynamically unstable motion of reentry capsule, AIAA Paper, 2589 (2000) 2000.
[18] S.E. Cliff, S.D. Thomas, The apollo capsule optimization for improved stability and omputational/experimental data comparisons, NASA TM-213457, (2005).
[19] H. Zhang, Z. Zhang, X. Yuan, W. Liu, Y. Xie, Y. Ye,Physical analysis and numerical simulation for the dynamic behaviour of vehicles in pitching oscillations or rocking motions, Science in China Series E:Technological Sciences, 50(4) (2007) 385-401.
[20] C.D. Kazemba, R.D. Braun, I.G. Clark, M.Schoenenberger, Survey of blunt body dynamic stability in supersonic flow, in: AIAA Atmospheric Flight Mechanics Conference, Minnesota, USA, 2012.
[21] C.D. Kazemba, R.D. Braun, M. Schoenenberger, I.G.Clark, Dynamic stability analysis of blunt-body entry vehicles using time-lagged aftbody pitching moments,Journal of Spacecraft and Rockets, 52(2) (2015) 393-403.
[22] D. Sugimoto, H. Nagai, K. Asai, K. Hiraki, Experimental study on dyanmics instability of re-entry capsule-shaped body using pressure sensitive paint, in: 48th AIAA aerospace sciences meeting, 2010.
[23] P.N. Desai, R.A. Mitcheltree, and F. McNeil, Cheatwood sample returns missions in the coming decade, 51st International Astronautical Congress, Brazil, 2000.
[24] M. Shakeri, Dynamic Stability Analysis of a Reentry Space Capsule in Pitching Motion with Free and Forced Oscillations, Master of Science thesis, Aerospace Research Institute, 2014.
[25] R. Kamali moghadam, M. Shakeri, Dynamic stability analysis of a conic reentry space capsoul in pitching motion with free and forced oscillations, in: 23th ISME Conference, Tehran, Iran, 2015.
[26] K. Hiraki, Y. Inatani, N. Ishii, T. Nakajima, M.Hinada, Dynamic stability of Muses-C capsule, in:21st international symposium on space technology and science, Omiyo, Japan, 1998.
[27] A. Davari, M. Soltani, Effects of plunging motion on unsteady aerodynamic behavior of an aircraft model in compressible flow, Iranian Journal of Science and Technology, 31(B1) (2007) 49.
[28] F. Rasi marzabadi, R. Kamali moghadam, Longitudinal dynamic derivatives of an airfoil under pitching and plunging oscillations in wind tunnel, Modares Mechanic Engineering Journal, 14(10) (2014) 159-166.
[29] M. Schroenenberger, L. Yates, W. Hathaway, Dynamic stability testing of the mars science laboratory entry capsule, AIAA Paper, 3917 (2009) 2009.
[30] B. Smith, R.D. Braun, I.G. Clark, Oscillation of supersonic inflatable aerodynamic decelerators at Mars, Master of Science Thesis, Georgia Institute of Technology, 2010.
[31] I.G. Clark, Aerodynamic design, analysis, and validation of a supersonic inflatable decelerator, PhD Thesis, Georgia Institute of Technology, 2009.
[32] R. Kamali moghadam, TLNS-PNS dual-code for efficient computing hypersonic equilibrium xisymmetric flows over blunt bodies, Master of Science Thesis, Sharif University of Technology, 2006.