-
1
-
-
34250853858
-
Effect of solid-rocket propellant formulations and exhaust-gas chemistries on the erosion of graphite nozzles
-
Palo Alto, CA, AIAA Paper, 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, Palo Alto, CA, AIAA Paper, 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/prep. 19770020304
-
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/prep. 19770020304
-
(1977)
Propellants and Explosives
, vol.2
, Issue.3
, pp. 55-63
-
-
Klager, K.1
-
3
-
-
35948943759
-
The prediction of graphite rocket nozzle recession rates
-
New Orleans, LA, Chemical Propulsion Information Agency, Publication 342, Columbia, MD, May
-
Geisler, R. L., "The Prediction of Graphite Rocket Nozzle Recession Rates", 1981 JANNAF Propulsion Meeting, New Orleans, LA, Chemical Propulsion Information Agency, Publication 342, Vol. 5, Columbia, MD, May 1981, pp. 173-196.
-
(1981)
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
-
-
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
-
6
-
-
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
-
7
-
-
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
-
8
-
-
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
-
(2007)
Journal of Propulsion and Power
, vol.23
, Issue.6
, pp. 1242-1254
-
-
Acharya, R.1
Kuo, K.K.2
-
9
-
-
84856861496
-
Numerical simulation of graphite nozzle erosion with parametric analysis
-
Acharya, R., and Kuo, K. K., "Numerical Simulation of Graphite Nozzle Erosion with Parametric Analysis", AIAA Paper 2010-6846, 2010.
-
(2010)
AIAA Paper 2010-6846
-
-
Acharya, R.1
Kuo, K.K.2
-
10
-
-
78651538361
-
Effect of kinetic schemes on graphite rocket nozzle erosion rates
-
doi:10.1615/IntJEnergeticMaterialsChemProp. v9.i1.50
-
Acharya, R., and Kuo, K. K., "Effect of Kinetic Schemes on Graphite Rocket Nozzle Erosion Rates", International Journal of Energetic Materials and Chemical Propulsion, Vol. 9, 2010, p. 71-90. doi:10.1615/ IntJEnergeticMaterialsChemProp. v9.i1.50
-
(2010)
International Journal of Energetic Materials and Chemical Propulsion
, vol.9
, pp. 71-90
-
-
Acharya, R.1
Kuo, K.K.2
-
11
-
-
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
-
12
-
-
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
-
13
-
-
77957830880
-
Effect of surface roughness and radiation on graphite nozzle erosion in solid rocket motors
-
Thakre, P., and Yang, V., "Effect of Surface Roughness and Radiation on Graphite Nozzle Erosion in Solid Rocket Motors", AIAA Paper 2009-5275, 2009.
-
(2009)
AIAA Paper 2009-5275
-
-
Thakre, P.1
Yang, V.2
-
14
-
-
84866694299
-
Mechanical erosion of nozzle material in solid-propellant rocket motors
-
Thakre, P., and Yang, V., "Mechanical Erosion of Nozzle Material in Solid-Propellant Rocket Motors", AIAA Paper 2010-615, 2010.
-
(2010)
AIAA Paper 2010-615
-
-
Thakre, P.1
Yang, V.2
-
15
-
-
67650863460
-
Coupled analysis of flowand surface ablation in carbon-carbon rocket nozzles
-
doi:10.2514/1.40197
-
Bianchi, D., Nasuti, F., and Martelli, E., "Coupled Analysis of Flowand 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
-
16
-
-
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
-
17
-
-
35748945167
-
A numerical approach for high-temperature flows over ablating surfaces
-
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)
AIAA Paper 2007-4537
-
-
Bianchi, D.1
Nasuti, F.2
Martelli, E.3
Onofri, M.4
-
18
-
-
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
-
19
-
-
0004079116
-
-
AIAA, Reston, VA
-
Anderson, J. D., Hypersonic and High Temperature Gas Dynamics, AIAA, Reston, VA, 2000, pp. 611-617.
-
(2000)
Hypersonic and High Temperature Gas Dynamics
, pp. 611-617
-
-
Anderson, J.D.1
-
20
-
-
0003592561
-
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 Rept. 1311, 1994.
-
(1994)
NASA Rept. 1311
-
-
Gordon, S.1
McBride, B.J.2
-
21
-
-
0003944113
-
-
Wiley, New York
-
Bird, R. B., Stewart, W. E., and Lightfoot, E. D., Transport Phenomena, Wiley, New York, 1960, pp. 563-572.
-
(1960)
Transport Phenomena
, pp. 563-572
-
-
Bird, R.B.1
Stewart, W.E.2
Lightfoot, E.D.3
-
22
-
-
84982318991
-
Multi-component diffusion with application to computational aerothermodynamics
-
Albuquerque, NM, AIAA Paper 1998-2575
-
Sutton, K., and Gnoffo, P. A., "Multi-Component Diffusion with Application to Computational Aerothermodynamics", 7th AIAA/ASME Joint Thermophysics and Heat Transfer Conference, Albuquerque, NM, AIAA Paper 1998-2575, 1998.
-
(1998)
7th AIAA/ASME Joint Thermophysics and Heat Transfer Conference
-
-
Sutton, K.1
Gnoffo, P.A.2
-
23
-
-
0024765297
-
Aerothermochemical analysis of carbon-carbon nozzle regression in solid-propellant rocket motors
-
doi:10.2514/3.23204
-
Borie, V., Brulard, J., and Lengelle, G., "Aerothermochemical Analysis of Carbon-Carbon Nozzle Regression in Solid-Propellant Rocket Motors", Journal of Propulsion and Power, Vol. 5, No. 6, 1989, pp. 665-673. doi:10.2514/3.23204
-
(1989)
Journal of Propulsion and Power
, vol.5
, Issue.6
, pp. 665-673
-
-
Borie, V.1
Brulard, J.2
Lengelle, G.3
-
24
-
-
17144374807
-
An analysis of the chemically reacting boundary layer and charring ablator. Part II: Finite difference solutions for the in-depth response of charring materials considering surface chemical and energy balances
-
Moyer, C. B., and Rindal, R. A., "An Analysis of the Chemically Reacting Boundary Layer and Charring Ablator. Part II: Finite Difference Solutions for the In-Depth Response of Charring Materials Considering Surface Chemical and Energy Balances", NASACR 1061, 1968.
-
(1968)
NASACR 1061
-
-
Moyer, C.B.1
Rindal, R.A.2
-
25
-
-
85002588700
-
Quasi-steady solution for ablation-erosion heat transfer
-
doi:10.2514/3.29938
-
Quan, V., "Quasi-Steady Solution for Ablation-Erosion Heat Transfer", Journal of Spacecraft and Rockets, Vol. 7, 1970, pp. 355-357. doi:10.2514/3.29938
-
(1970)
Journal of Spacecraft and Rockets
, vol.7
, pp. 355-357
-
-
Quan, V.1
-
26
-
-
84866713790
-
-
Rome, Jan
-
Bianchi, D., Modeling of Ablation Phenomena in Space Applications, Ph. D. Dissertation, Univ. Degli Studi di Roma "La Sapienza", Rome, Jan. 2008.
-
(2008)
Modeling of Ablation Phenomena in Space Applications, Ph. D. Dissertation, Univ. Degli Studi di Roma "La Sapienza"
-
-
Bianchi, D.1
-
27
-
-
0023089850
-
A technique for integrating two-dimensional euler equations
-
doi:10.1016/0045-7930 87 90005-3
-
Moretti, G., "A Technique for Integrating Two-Dimensional Euler Equations", Computers and Fluids, Vol. 15, No. 1, 1987, pp. 59-75. doi:10.1016/0045-7930 (87) 90005-3
-
(1987)
Computers and Fluids
, vol.15
, Issue.1
, pp. 59-75
-
-
Moretti, G.1
-
28
-
-
0000274787
-
Analysis of unsteady supersonic viscous flows by a shock fitting technique
-
doi:10.2514/3.13249
-
Nasuti, F., and Onofri, M., "Analysis of Unsteady Supersonic Viscous Flows by a Shock Fitting Technique", AIAA Journal, Vol. 34, No. 7, 1996, pp. 1428-1434. doi:10.2514/3.13249
-
(1996)
AIAA Journal
, vol.34
, Issue.7
, pp. 1428-1434
-
-
Nasuti, F.1
Onofri, M.2
-
29
-
-
0027988926
-
A one-equation turbulence model for aerodynamic flow
-
Spalart, P. R., and Allmaras, S. R., "A One-Equation Turbulence Model for Aerodynamic Flow", La Recherche Aerospatiale: Bulletin Bimestriel de l'Office National D'etudes et de Recherches Aerospatiales, Vol. 1, 1994, pp. 5-21.
-
(1994)
La Recherche Aerospatiale: Bulletin Bimestriel de l'Office National d'Etudes et de Recherches Aerospatiales
, vol.1
, pp. 5-21
-
-
Spalart, P.R.1
Allmaras, S.R.2
|