1 |
C. L. Chen, S. R. Chakravarthy and C. M. Hung, "Numerical Investigat ion of SeparatedNozzle Flows", AIAA, vol. 32, no. 9, 1994, pp.1836-1743
DOI
ScienceOn
|
2 |
F. Nasuti and M. Onofri, "Viscous andInviscid Vortex Generation During Startup ofRocket Nozzle", AIAA, vol. 36, no. 5, 1998, pp.809-815
DOI
ScienceOn
|
3 |
J. R. Edwards, "A Low-DiffusionFlux-Splitting Scheme for Navier-StokesCalculations", Computer & Fluids, vol. 26, no.6, 1997, pp. 635-659
DOI
ScienceOn
|
4 |
T. H. Pulliam (Senior Staff Scientist, FluidDynamics Division NASA Ames ResearchCenter), "Time Accuracy and The Use ofImplicit Methods" AIAA Paper 93-3360
|
5 |
R. F. Cuffel, L. H. Back, and P. F.Massier, " Transonic Flowfield in a SupersonicNozzle with Small Throat Radius of Curvature", AIAA, vol. 7, No.7, 1969, pp. 1364-1366
DOI
|
6 |
김희경, "압력비에 따른 박리 노즐 유동의 수치적 해석", 석사학위논문, 한국과학기술원, 2001
|