삭마 및 열분해 반응을 고려한 고체 추진기관의 열해석

목차 (Table of Contents)

• ABSTRACT
• 초록
• 1. 서론
• 2. 이론적 배경
• 3. 실험 및 고찰
• 4. 결론
• 참고문헌

참고문헌 (Reference)

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2 Aerotherm, "User's Manual Aerotherm Chemical Equilibrium(ACE) Computer Program"

3 Aerotherm, "User's Manual Aerotherm Charring Material Thermal Response AND Ablation Program"

4 MSC.Software Corporation, "User Subroutine AND Special Routines, Vol. D"

5 Ted B.Wertheimer, "Thermal Stress Analysis of TPS using Marc"

6 Fabrice Laturelle, "Thermal Decomposition Analysis of Rocket Motors and Other thremal Protection Systems using MSC-Marc-ATAS" 2003

7 MSC.Software Corporation, "Theory AND User Information, Vol. A"

8 M.E.Boyle, "The effect of high heating rate on pyrolysis of carbon/phenolic composites"

9 Boyarintsev,V. I, "The Ablation of Graphite in the Turbulent Flow of a Reacting Gas"

10 E. Y. WONG, "SOLID ROCKET NOZZLE DESIGN SUMMARY" Aerojet-General Corporation

11 Keiichi ISHIKO, "Implicit LES of Compressible Turbulent Flow over a Backward Facing Step in the nozzle of solid rocket motor" AIAA 2010

12 A.S.Koroteyev, "Gas Dynamics and Thermophysical Processes in Solid Rocket Propulsions"

13 KOBAYASHI Hideo, "Failed Launching of H-ⅡA Rocket #6, Failure Knowledge Database /100 Selected Cases"

14 J.B.Henderson, "Determination of kinetic parameters for the thermal decomposition of phenolic ablative materials by a multiple heating rate method" 44 : 253-264, 1981

15 Bonnie J. McBride, "Computer Program for Calculation of Complex Chemical Equilibrium Compositions AND Applications" Lewis Research Center, NASA 1996

16 Sergey Vyazovkin, "A unified approach to kinetic processing of nonisothermal data" 28 : 95-101, 1996

17 Bartz, D. R, "A Simple Equation for Rapid Estimation of Rocket Nozzle Convective HeatTransfer Coefficients" 27 (27): 49-51, 1957