참고문헌
- Carandente, V. (2014), "Aerthermodynamic and mission analyses of deployable aerobraking earth re-entry systems", Ph.D. Dissertation.
- Carandente, V., Elia, G. and Savino, R. (2013), "Conceptual design of de-orbit and re-entry modules for standard cubesats", Proceedings of the 2nd IAA Conference on University Satellite Missions and Cubesat Workshop, Rome, February.
- Carandente, V. and Savino, R. (2014), "New concepts of deployable de-orbit and re-entry systems for cubesat miniaturized satellites", Rec. Pat. Eng., 8(1), 2-12. https://doi.org/10.2174/1872212108666140204004335
- Carandente, V., Savino, R., D'Oriano, V. and Fortezza, R. (2014), "Deployable aerobraking earth entry systems for recoverable microgravity experiments", Proceedings of the 65th International Astronautical Congress, Toronto, Canada, September.
- Carandente, V., Savino, R., Iacovazzo, M. and Boffa, C. (2013), "Aerothermal analysis of a sample-return reentry capsule", Flu. Dyn. Mater. Proc., 9(4), 461-484.
- Carandente, V., Zuppardi, G. and Savino, R. (2014), "Aerothermodynamic and stability analyses of a deployable re-entry capsule", Acta Astronaut., 93, 291-303. https://doi.org/10.1016/j.actaastro.2013.07.030
- Dillman, R., DiNonno, J., Bodkin, R., Gsell, V., Miller, N., Olds, A. and Bruce, W. (2013), "Flight performance of the inflatable reentry vehicle experiment 3", Proceedings of the 10th International Planetary Probe Workshop, San Jose, U.S.A., June.
- Dillman, R., DiNonno, J., Bodkin, R., Gsell, V., Miller, N., Olds, A. and Bruce, W. (2010), "Flight performance of the inflatable reentry vehicle experiment II", Proceedings of the International Planetary Probe Workshop, Barcelona, Spain, June.
- Dowell, E. (1970), "Panel flutter: A review of aeroelastic stability of plates and shells", AIAA J., 8(3), 385-399. https://doi.org/10.2514/3.5680
- Dowell, E. (1975), Aeroelasticity of Plates and Shells, Springer, New York, U.S.A.
- Dugundji, J. (1966), "Theoretical considerations of panel flutter at high supersonic mach numbers", AIAA J., 4(7), 1257-1266. https://doi.org/10.2514/3.3657
- Ellen, C. (1965), "Approximate solution of the membrane flutter problem", AIAA J., 3(6), 1186-1187. https://doi.org/10.2514/3.3096
- Goldman, B. and Dowell, E. (2014), "Nonlinear oscillations of a fluttering plate resting on a unidirectional elastic foundation", AIAA J., 52(10), 2364-2368. https://doi.org/10.2514/1.J053290
- Goldman, B., Dowell, E. and Scott, R. (2013), "Flutter analysis of the thermal protection layer on the NASA HIAD", Proceedings of the 22nd AIAA Aerodynamic Decelerator Systems (ADS) Conference, Florida, U.S.A.
- Goldman, B., Dowell, E. and Scott, R. (2014), "In-flight aeroelastic stability of the thermal protection system on the NASA HIAD, part I: Linear theory", Proceedings of the 55th AIAA/ASMe/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference, Maryland, U.S.A.
- Goldman, B., Dowell, E. and Scott, R. (2015), "In-flight aeroelastic stability of the thermal protection system on the NASA HIAD, part II: Nonlinear theory and extended aerodynamics", Proceedings of the 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Florida, U.S.A.
- Goldman, B., Scott, R. and Dowell, E. (2014), Nonlinear Aeroelastic Analysis of the HIAD TPS Coupon in the NASA 8' High Temperature Tunnel: Theory and Experiment, NASA TM-2014-218267.
- Guruswamy , G. (2002), "A review of numerical fluids/structures interface methods for computations using high-fidelitynequations", Comput. Struct., 80(1), 31-41. https://doi.org/10.1016/S0045-7949(01)00164-X
- Hughes, S., Dillman, R., Starr, B., Stephan, R., Lindell, M., Player, C. and Cheatwood, F. (2005), "Inflatable re-entry vehicle experiment (IRVE) design overview", Proceedings of the 18th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, Munich, Germany, May.
- Johns, D. (1971), "Supersonic membrane flutter", AIAA J., 9(5), 960-961. https://doi.org/10.2514/3.6309
- Kramer, R., Cirak, F. and Pantano, C. (2013), "Fluid-structure interaction simulations of a tension-cone inflatable aerodynamic decelerator", AIAA J., 51(7), 1640-1656. https://doi.org/10.2514/1.J051939
- McNamara, J. and Friedmann, P. (2007), Aeroelastic and Aerothermoelastic Analysis of Hypersonic Vehicles: Current Status and Future Trends, Collection of Technical Papers-AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 3814.
- McNamara, J. and Friendmann, P. (2011), "Aeroelastic and aerothermoelastic analysis in hypersonic flows: Past, present, and future", AIAA J., 49(6), 1089-1122. https://doi.org/10.2514/1.J050882
- Mei, C., Abdel-Motagaly, K. and Chen, R. (1999), "Review of nonlinear panel flutter at supersonic and hypersonic speeds", Appl. Mech. Rev., 52(10), 321-332. https://doi.org/10.1115/1.3098919
- Rohrschneider, R. (2007), "Variable-fidelity hypersonic aeroelastic analysis of thin-film ballutes for aerocapture", Ph.D. Dissertation, Georgia Institute of Technology, U.S.A.
- Savino, R. (2013), "Study and development of a sub-orbital reentry demonstrator", Proceedings of the Italian Association of Aeronautics and Astronautics XXII Conference, Naples, Italy, September.
- Savino, R. and Carandente, V. (2012), "Aerothermodynamic and feasibility study of a deployable aerobraking re-entry capsule", Flu. Dyn. Mater. Process., 8(4), 453-477.
- Scott, R., Bartels, R. and Kandil, O. (2007), "An aeroelastic analysis of a thin flexible membrane", Proceedings of the 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Hawaii, U.S.A.
- Spriggs, J., Messiter, A. and Anderson, W. (1969), "Membrane flutter paradox-an explanation by singular perturbation methods", AIAA J., 7(9), 1704-1709. https://doi.org/10.2514/3.5379
- Wang, Z., Yang, S., Liu, D., Wang, X., Mignolet, M. and Bartels, R. (2010), Nonlinear Aeroelastic Analysis for a Wrinkling Aeroshell/Ballute System, Collection of Technical Papers-AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
- Wilde, D. and Walther, S. (2001), "Inflatable re-entry and descent technology (IRDT)-further developments", Proceedings of the 2nd International Symposium of Atmospheric Re-entry Vehicles and Systems, Arcachon, France.
피인용 문헌
- Coupled Fluid-Structural Thermal Numerical Methods for Thermal Protection System vol.57, pp.8, 2017, https://doi.org/10.2514/1.j057616