[1] Schulte G. Fuel regression and flame stabilization studies of solid-fuel ramjets[J]. Journal of Propulsion, 1986,6(4):301-304.
[2]
[2] Amnon N, Alon G. Burning and flameholding characteristics of a miniature solid fuel ramjet combustor[J]. Journal of Propulsion and Power, 1991, 7(3): 357-363.
[3]
[3] Elands P J M, Korting P A O G, Dijkstra F. Combustion of polyethylene in a solid fuel ramjet-A comparison of computational and experimental results[C]∥AIAA/ASME/SAE/ASEE 24th Joint Propulsion Conference. Boston, Massachusetts: AIAA/ASME/SAE/ASEE, 1988.
[4]
[4] Elands P J M, Dijkstra F. Validation of the flow and combustion processes in a solid fuel ramjet[C]∥AIAA/ASME/SAE/ASEE 24th Joint Propulsion Conference. Sacrameto, CA: AIAA/ASME/SAE/ASEE,1991.
[5]
[5] Zvuloni R, Gany A, Levy Y, et al. Geometric effects on the combustion in solid fuel ramjets[J]. Journal of Propulsion, 1989, 5(1): 32-37.
[6]
[8] Mawid M A, Sekar B. Kinetic modeling of ethylene oxidation in high speed reacting flows, AIAA 97-3269[R]. US: AIAA, 1997.
[7]
[9] Gobbo Ferrrira J. Performance of an experimental polyethylene solid fuel ramjet[J]. Acta Astronautica, 1999, 45(1): 11-18.
[8]
[10] Yang J T, Wu C Y Y. Controlling mechanisms of ignition of solid fuel in a sudden-expansion combustor[J]. Journal of Propulsion and Power, 1995, 11(3): 483-488.
[9]
[11] Tahsini A M, Farshchi M. Igniter jet dynamics in solid fuel ramjets[J]. Acta Astronautica, 2009, 64(3):166-175.
[10]
[12] 夏强. 固体燃料冲压发动机工作过程研究[D]. 南京: 南京理工大学, 2011.
[11]
[13] Amnon N, Alon G. Burning and flameholding characteristics of a miniature solid fuel ramjet combustor[J]. Journal of Propulsion and Power, 1991, 7(3): 357-363.
[12]
[14] Witt M A. Investigation into the feasibility of using solid fuel ramjets for high supersonic/low hypersonic tactical missiles, ADA214737[R]. Monterey, CA: Naval Postgraduate School, 1989.
[7] Wilde J P. Fuel pyrolysis effects on hybrid rocket and solid fuel ramjet combustor performance [D].Delft,Netherlands: Delft
[15]
[15] Angus W J. An investigation into the performance characteristics of a solid fuel scramjet propulsion device,ADA246486[R].Monterey, CA: Naval Postgraduate School, 1991.