Year |
Citation |
Score |
2017 |
Acharya R, Evans B, Pitt J, Costanzo F, Kuo KK. COUPLING OF TRANSIENT THERMAL AND MECHANICAL STRESSES COMPUTATIONS IN GRAPHITE NOZZLE MATERIALS International Journal of Energetic Materials and Chemical Propulsion. 16: 175-195. DOI: 10.1615/Intjenergeticmaterialschemprop.2018024875 |
0.473 |
|
2010 |
Essel JT, Acharya R, Sabourin JL, Zhang B, Kuo KK, Yetter RA. High-temperature behavior of graphite under laser irradiation International Journal of Energetic Materials and Chemical Propulsion. 9: 205-218. DOI: 10.1615/Intjenergeticmaterialschemprop.V9.I3.20 |
0.498 |
|
2010 |
Acharya R, Kuo KK. Effect Of Reaction Kinetic Schemes On Graphite Rocket Nozzle Erosion Rates International Journal of Energetic Materials and Chemical Propulsion. 9: 71-90. DOI: 10.1615/Intjenergeticmaterialschemprop.V9.I1.50 |
0.499 |
|
2010 |
Acharya R, Kuo K. Implementation of approximate riemann solver to two-phase flows in mortar systems Journal of Applied Mechanics, Transactions Asme. 77: 1-5. DOI: 10.1115/1.4001558 |
0.489 |
|
2009 |
Kuo KK, Acharya R, Boyd E, Thynell ST. Pyrolysis/evaporation study of succinic acid/polyvinyl acetate for reducing nozzle erosion Journal of Propulsion and Power. 25: 801-807. DOI: 10.2514/1.37508 |
0.537 |
|
2009 |
Moore JD, Kuo KK, Acharya R, Ferrara PJ. EFFECT OF FLASH-TUBE VENT-HOLE PATTERNS ON THE COMBUSTION PRODUCT DISCHARGE RATE International Journal of Energetic Materials and Chemical Propulsion. 8: 199-220. DOI: 10.1615/Intjenergeticmaterialschemprop.V8.I3.30 |
0.518 |
|
2008 |
Acharya R, Kuo KK. Graphite Rocket Nozzle Erosion Rate Reduction By Boundary-Layer Control Using Ablative Materials At High Pressures International Journal of Energetic Materials and Chemical Propulsion. 7: 399-419. DOI: 10.1615/Intjenergeticmaterialschemprop.V7.I5.40 |
0.518 |
|
2008 |
Acharya R, Kuo KK. Effect Of Different Flash-Tube Vent-Hole Patterns On Interior Ballistic Processes Of Ignition Cartridge Of 120-Mm Mortar System International Journal of Energetic Materials and Chemical Propulsion. 7: 383-397. DOI: 10.1615/Intjenergeticmaterialschemprop.V7.I5.30 |
0.5 |
|
2007 |
Acharya R, Kuo KK. Effect of pressure and propellant composition on graphite rocket nozzle erosion rate Journal of Propulsion and Power. 23: 1242-1254. DOI: 10.2514/1.24011 |
0.54 |
|
2007 |
Kuo KK, Acharya R, Ferrara PJ, Moore JD. METHOD OF CHARACTERISTICS SIMULATION OF INTERIOR BALLISTIC PROCESSES OF M1020 IGNITION CARTRIDGEIN A 120-mm MORTAR SYSTEM International Journal of Energetic Materials and Chemical Propulsion. 6: 629-650. DOI: 10.1615/Intjenergeticmaterialschemprop.V6.I5.60 |
0.479 |
|
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