-
1
-
-
34250853858
-
Effect of solid-rocket propellant formulations and exhaust-gas chemistries on the erosion of graphite nozzles
-
CPIA Publ., Palo Alto, CA, Jan
-
Swope, L. W., and Berard, M. F., "Effect of Solid-Rocket Propellant Formulations and Exhaust-Gas Chemistries on the Erosion of Graphite Nozzles," AIAA Solid Propellant Rocket Conference, CPIA Publ., Palo Alto, CA, Jan. 1964.
-
(1964)
AIAA Solid Propellant Rocket Conference
-
-
Swope, L.W.1
Berard, M.F.2
-
2
-
-
84983897618
-
The interaction of the efflux of solid propellants with nozzle materials
-
doi:10.1002/(ISSN)1521-4087
-
Klager, K., "The Interaction of the Efflux of Solid Propellants with Nozzle Materials," Propellants and Explosives, Vol. 2, No. 3, 1977, pp. 55-63. doi:10.1002/(ISSN)1521-4087
-
(1977)
Propellants and Explosives
, vol.2
, Issue.3
, pp. 55-63
-
-
Klager, K.1
-
3
-
-
35948943759
-
The prediction of graphite rocket nozzle recession rates
-
The Johns HopkinsUniv.Applied Physics Lab.,Maryland,May
-
Geisler, R. L., "The Prediction of Graphite Rocket Nozzle Recession Rates," The 1981 JANNAF Propulsion Meeting, Vol. 5, The Johns HopkinsUniv.Applied Physics Lab.,Maryland,May 1981, pp. 173-196.
-
(1981)
The 1981 JANNAF Propulsion Meeting
, vol.5
, pp. 173-196
-
-
Geisler, R.L.1
-
4
-
-
84888742982
-
A Comprehensive theoretical model for carbon-carbon composite recession
-
doi:10.1080/00102208508960374
-
Kuo, K. K., and Keswani, S. T., "A Comprehensive Theoretical Model for Carbon-Carbon Composite Recession," Combustion Science and Technology, Vol. 42, Nos. 3-4, 1985, pp. 145-164. doi:10.1080/00102208508960374
-
(1985)
Combustion Science and Technology
, vol.42
, Issue.3-4
, pp. 145-164
-
-
Kuo, K.K.1
Keswani, S.T.2
-
5
-
-
0003583351
-
-
Wiley, New York, NY
-
Sutton, G. P., and Biblarz, O., Rocket Propulsion Elements,Wiley, New York, NY, 2001, pp. 550-563.
-
(2001)
Rocket Propulsion Elements
, pp. 550-563
-
-
Sutton, G.P.1
Biblarz, O.2
-
6
-
-
34249047914
-
-
AIAA Paper 2006-4936
-
Koo, J. H., Ho, D.W. H., and Ezekoye, O. A., "A Review of Numerical and Experimental Characterization of Thermal Protection Materials: Part 1. Numerical Modeling," AIAA Paper 2006-4936, 2006.
-
(2006)
A Review of Numerical and Experimental Characterization of Thermal Protection Materials: Part 1. Numerical Modeling
-
-
Koo, J.H.1
Ho, D.W.H.2
Ezekoye, O.A.3
-
7
-
-
0347957955
-
A Semiquantitative prediction of the erosion of graphite nozzle inserts
-
doi:10.2514/3.2570
-
Delaney, L. J., Eagleton, L. C., and Jones, W. H., "A Semiquantitative Prediction of the Erosion of Graphite Nozzle Inserts," AIAA Journal, Vol. 2, No. 8, 1964, pp. 1428-1433. doi:10.2514/3.2570
-
(1964)
AIAA Journal
, vol.2
, Issue.8
, pp. 1428-1433
-
-
Delaney, L.J.1
Eagleton, L.C.2
Jones, W.H.3
-
8
-
-
84862638841
-
Erosion of graphite in solid- propellant combustion gases and effects on heat transfer
-
doi:10.2514/3.3117
-
McDonald, A. J., and Hedman, P. O., "Erosion of Graphite in Solid- Propellant Combustion Gases and Effects on Heat Transfer," AIAA Journal, Vol. 3, No. 7, 1965, pp. 1250-1257. doi:10.2514/3.3117
-
(1965)
AIAA Journal
, vol.3
, Issue.7
, pp. 1250-1257
-
-
McDonald, A.J.1
Hedman, P.O.2
-
9
-
-
84954700426
-
Validation of an aerothermochemical model for graphite nozzle recession and heat-transfer processes
-
doi:10.1080/00102208608923872
-
Keswani, S. T., and Kuo, K. K., "Validation of an Aerothermochemical Model for Graphite Nozzle Recession and Heat-Transfer Processes," Combustion Science and Technology,Vol. 47, Nos. 3-4, 1986, pp. 177- 192. doi:10.1080/00102208608923872
-
(1986)
Combustion Science and Technology
, vol.47
, Issue.3-4
, pp. 177-192
-
-
Keswani, S.T.1
Kuo, K.K.2
-
10
-
-
36849019047
-
Effect of pressure and propellant composition on graphite rocket nozzle erosion rate
-
DOI 10.2514/1.24011
-
Acharya, R., and Kuo, K. K., "Effect of Pressure and Propellant Composition on Graphite Rocket Nozzle Erosion Rate," Journal of Propulsion and Power, Vol. 23, No. 6, 2007, pp. 1242-1254. doi:10.2514/1.24011 (Pubitemid 350218819)
-
(2007)
Journal of Propulsion and Power
, vol.23
, Issue.6
, pp. 1242-1254
-
-
Acharya, R.1
Kuo, K.K.2
-
12
-
-
78651538361
-
Effect of reaction kinetic schemes on graphite rocket nozzle erosion rates
-
doi:10.1615/IntJEnergeticMaterialsChemProp.v9.i1.50
-
Acharya, R., and Kuo, K. K., "Effect of Reaction Kinetic Schemes on Graphite Rocket Nozzle Erosion Rates," International Journal of Energetic Materials and Chemical Propulsion, Vol. 9, No. 1, 2010, pp. 71-90. doi:10.1615/IntJEnergeticMaterialsChemProp.v9.i1.50
-
(2010)
International Journal of Energetic Materials and Chemical Propulsion
, vol.9
, Issue.1
, pp. 71-90
-
-
Acharya, R.1
Kuo, K.K.2
-
13
-
-
49249092022
-
Chemical erosion of carbon-carbon/ graphite nozzles in solid-propellant rocket motors
-
doi:10.2514/1.34946
-
Thakre, P., and Yang, V., "Chemical Erosion of Carbon-Carbon/ Graphite Nozzles in Solid-Propellant Rocket Motors," Journal of Propulsion and Power, Vol. 24, No. 4, 2008, pp. 822-833. doi:10.2514/1.34946
-
(2008)
Journal of Propulsion and Power
, vol.24
, Issue.4
, pp. 822-833
-
-
Thakre, P.1
Yang, V.2
-
14
-
-
63649147768
-
Chemical erosion of refractory-metal nozzle inserts in solid-propellant rocket motors
-
doi:10.2514/1.37922
-
Thakre, P., and Yang, V., "Chemical Erosion of Refractory-Metal Nozzle Inserts in Solid-Propellant Rocket Motors," Journal of Propulsion and Power, Vol. 25, No. 1, 2009, pp. 40-50. doi:10.2514/1.37922
-
(2009)
Journal of Propulsion and Power
, vol.25
, Issue.1
, pp. 40-50
-
-
Thakre, P.1
Yang, V.2
-
17
-
-
67650863460
-
Coupled analysis of flow and surface ablation in carbon-carbon rocket nozzles
-
doi:10.2514/1.40197
-
Bianchi, D., Nasuti, F., and Martelli, E., "Coupled Analysis of Flow and Surface Ablation in Carbon-Carbon Rocket Nozzles," Journal of Spacecraft and Rockets, Vol. 46, No. 3, 2009, pp. 492-500. doi:10.2514/1.40197
-
(2009)
Journal of Spacecraft and Rockets
, vol.46
, Issue.3
, pp. 492-500
-
-
Bianchi, D.1
Nasuti, F.2
Martelli, E.3
-
18
-
-
78650971551
-
Thermochemical erosion analysis for graphite/carbon-carbon rocket nozzles
-
doi:10.2514/1.47754
-
Bianchi, D., Nasuti, F., Onofri, M., and Martelli, E., "Thermochemical Erosion Analysis for Graphite/Carbon-Carbon Rocket Nozzles," Journal of Propulsion and Power, Vol. 27, No. 1, 2011, pp. 197-205. doi:10.2514/1.47754
-
(2011)
Journal of Propulsion and Power
, vol.27
, Issue.1
, pp. 197-205
-
-
Bianchi, D.1
Nasuti, F.2
Onofri, M.3
Martelli, E.4
-
19
-
-
84866696369
-
Carbon-carbon nozzle erosion and shape change in full-scale solid-rocket motors
-
doi:10.2514/1.58842
-
Bianchi, D., and Nasuti, F., "Carbon-Carbon Nozzle Erosion and Shape Change in Full-Scale Solid-Rocket Motors," Journal of Propulsion and Power, Vol. 28, No. 4, 2012, pp. 820-830. doi:10.2514/1.58842
-
(2012)
Journal of Propulsion and Power
, vol.28
, Issue.4
, pp. 820-830
-
-
Bianchi, D.1
Nasuti, F.2
-
21
-
-
84873859189
-
-
AIAA Paper 2012- 0533
-
Bianchi, D., Nasuti, F., and Onofri, M., "Radius of Curvature Effects on Throat Thermochemical Erosion in Solid Rocket Motors," AIAA Paper 2012-0533, 2012.
-
(2012)
Radius of Curvature Effects on Throat Thermochemical Erosion in Solid Rocket Motors
-
-
Bianchi, D.1
Nasuti, F.2
Onofri, M.3
-
22
-
-
29544444358
-
Navier-Stokes solutions with finite rate ablation for planetary mission earth reentries
-
DOI 10.1118/1.1861395
-
Chen,Y. K., and Milos, F. S., "Navier-Stokes Solutions with Finite Rate Ablation for Planetary Mission Earth Reentries," Journal of Spacecraft and Rockets, Vol. 42, No. 6, 2005, pp. 961-970. doi:10.2514/1.12248 (Pubitemid 43017335)
-
(2005)
Journal of Spacecraft and Rockets
, vol.42
, Issue.6
, pp. 961-970
-
-
Chen, Y.-K.1
Milos, F.S.2
-
24
-
-
84867491078
-
-
AIAA Paper 2011-3784
-
MacLean, M., Marschall, J., and Driver, D. M., "Finite-Rate Surface Chemistry Model, 2: Coupling to Viscous Navier-Stokes Code," AIAA Paper 2011-3784, 2011.
-
(2011)
Finite-Rate Surface Chemistry Model, 2: Coupling to Viscous Navier-Stokes Code
-
-
Maclean, M.1
Marschall, J.2
Driver, D.M.3
-
25
-
-
84877810433
-
A Numerical approach for the study of the gas-surface interaction in carbon- phenolic solid rocket nozzles
-
doi:10.1016/j.ast.2012.06.003
-
Turchi, A., Bianchi, D., Nasuti, F., and Onofri, M., "A Numerical Approach for the Study of the Gas-Surface Interaction in Carbon- Phenolic Solid Rocket Nozzles," Aerospace Science and Technology, Vol. 27, No. 1, 2013, pp. 25-31. doi:10.1016/j.ast.2012.06.003
-
(2013)
Aerospace Science and Technology
, vol.27
, Issue.1
, pp. 25-31
-
-
Turchi, A.1
Bianchi, D.2
Nasuti, F.3
Onofri, M.4
-
26
-
-
0007074523
-
Computer program for calculation of complex chemical equilibrium compositions and applications
-
Gordon, S., and McBride, B. J., "Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications," NASA RP-1311, 1994.
-
(1994)
NASA RP-1311
-
-
Gordon, S.1
McBride, B.J.2
-
27
-
-
0003944113
-
-
Wiley, New York, NY
-
Bird, R. B., Stewart,W. E., and Lightfoot, E. D., Transport Phenomena, Wiley, New York, NY, 1960, pp. 563-572.
-
(1960)
Transport Phenomena
, pp. 563-572
-
-
Bird, R.B.1
Stewart, W.E.2
Lightfoot, E.D.3
-
28
-
-
0042938945
-
-
NASA CR-1060
-
Kendall, R. M., Bartlett, E. P., Rindal, R. A., and Moyer, C. B., "An Analysis of the Chemically Reacting Boundary Layer and Charring Ablator. Part 1: Summary Report," NASA CR-1060, 1968.
-
(1968)
An Analysis of the Chemically Reacting Boundary Layer and Charring Ablator. Part 1: Summary Report
-
-
Kendall, R.M.1
Bartlett, E.P.2
Rindal, R.A.3
Moyer, C.B.4
-
29
-
-
0028132507
-
Review of numerical procedures for computational surface thermochemistry
-
doi:10.2514/3.497
-
Milos, F. S., and Rasky, D. J., "Review of Numerical Procedures for Computational Surface Thermochemistry," Journal of Thermophysics and Heat Transfer, Vol. 8, No. 1, 1994, pp. 24-34. doi:10.2514/3.497
-
(1994)
Journal of Thermophysics and Heat Transfer
, vol.8
, Issue.1
, pp. 24-34
-
-
Milos, F.S.1
Rasky, D.J.2
-
31
-
-
85172036622
-
-
AIAA Paper 2012-4318
-
Bianchi, D., Turchi, A., Nasuti, F., and Onofri, M., "Coupled CFD Analysis of Thermochemical Erosion and Unsteady Heat Conduction in Solid Rocket Nozzles," AIAA Paper 2012-4318, 2012.
-
(2012)
Coupled CFD Analysis of Thermochemical Erosion and Unsteady Heat Conduction in Solid Rocket Nozzles
-
-
Bianchi, D.1
Turchi, A.2
Nasuti, F.3
Onofri, M.4
-
32
-
-
85088339288
-
-
AIAA Paper 2013-0186
-
Turchi, A., Bianchi, D., Nasuti, F., and Onofri, M., "Radiation and Roughness Effects on the Thermochemical Erosion of Ablative Materials in Rocket Nozzles," AIAA Paper 2013-0186, 2013.
-
(2013)
Radiation and Roughness Effects on the Thermochemical Erosion of Ablative Materials in Rocket Nozzles
-
-
Turchi, A.1
Bianchi, D.2
Nasuti, F.3
Onofri, M.4
-
33
-
-
0029657111
-
Modeling of graphite oxidation in a stagnation-point flow field using detailed homogeneous and semiglobal heterogeneous mechanisms with comparisons to experiments
-
DOI 10.1016/0010-2180(95)00151-4
-
Chelliah, H. K., Makino, A., Kato, I., Araki, N., and Law, C. K., "Modeling of Graphite Oxidation in a Stagnant-Point Flow Field Using Detailed Homogeneous and Semiglobal Heterogeneous Mechanisms with Comparisons to Experiments," Combustion and Flame, Vol. 104, No. 4, 1996, pp. 469-480. doi:10.1016/0010-2180(95)00151-4 (Pubitemid 26103983)
-
(1996)
Combustion and Flame
, vol.104
, Issue.4
, pp. 469-480
-
-
Chelliah, H.K.1
Makino, A.2
Kato, I.3
Araki, N.4
Law, C.K.5
-
34
-
-
58149368494
-
The Oxidation of graphite powder in flame reactions zones
-
Combustion Inst., Pittsburgh, PA
-
Bradley, D., Dixon-Lewis, G., Habik, S. E., and Mushi, E. M., "The Oxidation of Graphite Powder in Flame Reactions Zones," Twentieth Symposium (International) on Combustion, Combustion Inst., Pittsburgh, PA, 1984, pp. 931-940.
-
(1984)
Twentieth Symposium (International) on Combustion
, pp. 931-940
-
-
Bradley, D.1
Dixon-Lewis, G.2
Habik, S.E.3
Mushi, E.M.4
-
35
-
-
78549279799
-
-
AIAA Paper 2009-261
-
Venkatachari, B. S., Cheng, B., and Koomullil, R., "Uncertainty Analysis of Surface Ablation," AIAA Paper 2009-261, 2009.
-
(2009)
Uncertainty Analysis of Surface Ablation
-
-
Venkatachari, B.S.1
Cheng, B.2
Koomullil, R.3
-
36
-
-
77958188009
-
Navier-stokes simulations of hypersonic flows with coupled graphite ablation
-
doi:10.2514/1.47995
-
Bianchi, D., Nasuti, F., and Martelli, E., "Navier-Stokes Simulations of Hypersonic Flows with Coupled Graphite Ablation," Journal of Spacecraft and Rockets, Vol. 47, No. 4, 2010, pp. 554-562. doi:10.2514/1.47995
-
(2010)
Journal of Spacecraft and Rockets
, vol.47
, Issue.4
, pp. 554-562
-
-
Bianchi, D.1
Nasuti, F.2
Martelli, E.3
-
37
-
-
35748945167
-
-
AIAA Paper 2007-4537
-
Bianchi, D., Nasuti, F., Martelli, E., and Onofri, M., "A Numerical Approach for High-Temperature Flows over Ablating Surfaces," AIAA Paper 2007-4537, 2007.
-
(2007)
A Numerical Approach for High-Temperature Flows over Ablating Surfaces
-
-
Bianchi, D.1
Nasuti, F.2
Martelli, E.3
Onofri, M.4
-
38
-
-
84878319832
-
Numerical analysis of nozzle material thermochemical erosion in hybrid rocket engines
-
doi:10.2514/1.B34813
-
Bianchi, D., and Nasuti, F., "Numerical Analysis of Nozzle Material Thermochemical Erosion in Hybrid Rocket Engines," Journal of Propulsion and Power, Vol. 29, No. 3, 2013, pp. 547-558. doi:10.2514/1.B34813
-
(2013)
Journal of Propulsion and Power
, vol.29
, Issue.3
, pp. 547-558
-
-
Bianchi, D.1
Nasuti, F.2
-
39
-
-
0027988926
-
AOne-equation turbulence model for aerodynamic flow
-
Spalart, P. R., and Allmaras, S. R., "AOne-Equation Turbulence Model for Aerodynamic Flow," La Recherche Aerospatiale, Vol. 1, 1994, pp. 5-21.
-
(1994)
La Recherche Aerospatiale
, vol.1
, pp. 5-21
-
-
Spalart, P.R.1
Allmaras, S.R.2
-
40
-
-
84885042630
-
-
AIAA Paper 1981-1461
-
Powers, L. B., Bailey, R. L., and Morrison, B. H., "Shuttle Solid Rocket Motor Nozzle Alternate Ablative Evaluation," AIAA Paper 1981-1461, 1981.
-
Shuttle Solid Rocket Motor Nozzle Alternate Ablative Evaluation
, vol.1981
-
-
Powers, L.B.1
Bailey, R.L.2
Morrison, B.H.3
-
41
-
-
0020100855
-
Shuttle subscaleablativenozzle tests
-
doi:10.2514/3.62217
-
Powers, L.B., and Bailey,R. L., "Shuttle SubscaleAblativeNozzle Tests," Journal of Spacecraft and Rockets, Vol. 19, No. 2, 1982, pp. 104-112. doi:10.2514/3.62217
-
(1982)
Journal of Spacecraft and Rockets
, vol.19
, Issue.2
, pp. 104-112
-
-
Powers, L.B.1
Bailey, R.L.2
-
42
-
-
0026622438
-
High temperature thermomechanical behavior of carbon-phenolic and carbon-carbon composites, 2. Results
-
doi:10.1177/002199839202600205
-
McManus, H., and Springer, G., "High Temperature Thermomechanical Behavior of Carbon-Phenolic and Carbon-Carbon Composites, 2. Results," Journal of Composite Materials, Vol. 26, No. 2, 1992, pp. 230-255. doi:10.1177/002199839202600205
-
(1992)
Journal of Composite Materials
, vol.26
, Issue.2
, pp. 230-255
-
-
McManus, H.1
Springer, G.2
-
45
-
-
84880842005
-
-
AIAA Paper 2010-7084
-
Bianchi, S., Serraglia, F., Giliberti, F., Betti, F., and Milana, C., "Vega Solid Rocket Motors Development and Qualification," AIAA Paper 2010-7084, 2010.
-
(2010)
Vega Solid Rocket Motors Development and Qualification
-
-
Bianchi, S.1
Serraglia, F.2
Giliberti, F.3
Betti, F.4
Milana, C.5
-
46
-
-
34249326906
-
-
AIAA Paper 2006-5243
-
Daimon, Y., Shimada, T., Tsuboi, N., Takaki, R., Fujita, K., and Takekawa, K., "Evaluation of Ablation and Longitudinal Vortices in Solid Rocket Motor by Computational Fluid Dynamics," AIAA Paper 2006-5243, 2006.
-
(2006)
Evaluation of Ablation and Longitudinal Vortices in Solid Rocket Motor by Computational Fluid Dynamics
-
-
Daimon, Y.1
Shimada, T.2
Tsuboi, N.3
Takaki, R.4
Fujita, K.5
Takekawa, K.6
|