1 김경식, "폭압을 사용하는 연속조정 추진구조체의 열-구조해석" 한국전산구조공학회 24 (24): 699-706, 2011
2 Beastall, D., "Wind-tunnel Tests on Teo-dimensional Supersonic Aerofoils at M=1.86 and M=2.48" R&M 1950
3 Kauffmann, J., "Systems Analysis of a High Thrust, Low-Cost Rocket Engine" 1-7, 2001
4 "MPDB v7.37"
5 Incropera, F., "Introduction to Heat Transfer" Wiley 1985
6 Zucrow, M. J., "Gas Dynamics, Vol. 1" Wiley & Sons 233-234, 1997
7 John, J., "Gas Dynamics, In Pearson Int. Ed.3rd.ed" 350-351, 2006
8 Aksel, M. H., "Gas Dynamics" Prentice-Hall 342-344, 1994
9 Cowles, D. K., "Design of a Tomahawk Cruise Missile Booster Rocket Motor" Rensselaer Polytechnic Institute Hartford 2012
10 Ahmad, R. A., "Convective Heat Transfer in the Reusable Solid Rocket Motor of the Space Transportation System" 26 (26): 30-45, 2005
1 김경식, "폭압을 사용하는 연속조정 추진구조체의 열-구조해석" 한국전산구조공학회 24 (24): 699-706, 2011
2 Beastall, D., "Wind-tunnel Tests on Teo-dimensional Supersonic Aerofoils at M=1.86 and M=2.48" R&M 1950
3 Kauffmann, J., "Systems Analysis of a High Thrust, Low-Cost Rocket Engine" 1-7, 2001
4 "MPDB v7.37"
5 Incropera, F., "Introduction to Heat Transfer" Wiley 1985
6 Zucrow, M. J., "Gas Dynamics, Vol. 1" Wiley & Sons 233-234, 1997
7 John, J., "Gas Dynamics, In Pearson Int. Ed.3rd.ed" 350-351, 2006
8 Aksel, M. H., "Gas Dynamics" Prentice-Hall 342-344, 1994
9 Cowles, D. K., "Design of a Tomahawk Cruise Missile Booster Rocket Motor" Rensselaer Polytechnic Institute Hartford 2012
10 Ahmad, R. A., "Convective Heat Transfer in the Reusable Solid Rocket Motor of the Space Transportation System" 26 (26): 30-45, 2005
11 Mcbride, B. J., "An Intrim Updated Version of the NASA Lewis Computer Program for Calculating Complex Chemical Equilibria with Applications" NASA 1994
12 Hirai, K., "Ablation Analysis for Solid Rocket Motor Nozzles" 43 : 49-54, 2003
13 Bartz, D. R., "A Simple Equation for Rapid Estimation of Rocket Nozzle Convective Heat Transfer Coefficient" 27 (27): 49-51, 1957