Swirl coaxial atomization: Cold-flow and hot-fire experiments

33rd Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1995, Pages

  Rahman, S A ^a   Pal, S ^a   Santoro, R J ^a  

^a PENNSYLVANIA STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; ATOMIZATION; COMBUSTION CHAMBERS; COMPUTER SOFTWARE REUSABILITY; EXPLOSIVES; FLAMMABILITY TESTING; FLOW OF GASES; IGNITION; LIQUEFIED GASES; REUSABILITY; ROCKETS; VISUALIZATION;

CHAMBER PRESSURE; ENGINE TECHNOLOGY; FIRE EXPERIMENTS; GASEOUS HYDROGEN; RE-USABLE LAUNCH VEHICLES (RLV); ROCKET APPLICATIONS; ROCKET COMBUSTION CHAMBERS; SPRAY ATOMIZATION;

FIRES;

EID: 34250878785     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (24)

1. Moser, M. D., Merenich, J. J., Pal, S., and Santoro, R. J., "OH-Radical Imaging and Velocity Field Measurements in a Gaseous Hydrogen/Oxygen Rocket," AIAA Paper 93-2036, AIAA/SAE/ASME/ASEE 29th Joint Propulsion Conference & Exhibit, Monterey, CA., June 28-30, 1993.
2. Ryan, H. M III, Anderson, W. E„ Pal, S., and Santoro, R. J., "Atomization Characteristics of Impinging Liquid Jets," AIAA Paper 93-0230, 31st Aerospace Sciences Meeting & Exhibit, Reno, NV., Jan 11-14, 1993.
3. Pal, S., Moser, M. D., Ryan, H. M., Foust M. J., and Santoro, R. J., "Flowfield Characteristics in a Liquid Propellant Rocket," AIAA Paper 93-1882, AIAA/SAE/ASME/ASEE 29th Joint Propulsion Conference & Exhibit, Monterey, CA., June 28-30, 1993.
4. Beisler, M. A., Pal, S., Moser, M. D., and Santoro, R. J., "Shear Coaxial Injector Atomization in a LOX/GH2 Propellant Rocket," AIAA Paper 94-2775, AIAA/SAE/ASME/ASEE 30th Joint Propulsion Conference & Exhibit, Indianapolis, IN., June 27-29, 1994.
5. Brown, J. R., "Cryogenic Upper State Propulsion - RL10 and Derivative Engines," NASA Conference Publication 3112, Vol. 2, Space Transportation Propulsion Technology Symposium - Proceedings Vol. 2, held at Penn State University, State College, PA., June 25-29, 1990.
6. Andreyev, A. V., Chepkin, V., and Fanciullo, T. J., "Investigation of Oxygen/Hydrogen Combustion Stability in Staged Combustion Liquid Rocket Engines," AIAA/SAE/ASME/ASEE 30th Joint Propulsion Conference, Indianapolis, IN., June 28-30, 1994
7. Knuth, W. K., and Crawford, R. C, "Oxygen-Rich Combustion Process Applications and Benefits," AIAA Paper 91-2042, AIAA/SAE/ASME 27th Joint Propulsion Conference, Sacramento, CA., June 24-26,1991.
8. Anon., Liquid Rocket Engine Injectors, NASA SP-8089, March 1976.
9. Bailey, C. R., "A Preliminary Investigation of Oxidizer-Rich Hydrogen-Oxygen Combustion Characteristics," NASA TN D-3729, NASA Marshall Space Flight Center, December 1966.
10. Giffen, E., and Muraszew, A., The Atomisation of Liquid Fuels, Chapman & Hall, 1953, Ch. V.
11. Novikov, I.I., "Atomization of Liquids by Centrifugal Nozzles," (translated from Russian Journal of Technical Physics, Vol. 18, No. 3, 1948, pp 345-354) The Engineers' Digest, Vol. 10, No. 3, March 1949, pp 72-74.
12. Tate, R. W., and Marshall, W. R., Jr., "Atomization by Centrifugal Pressure Nozzles - Part I and II," Chemical Engineering Progress, Vol. 49, No. 4, April 1953, pp 169-174 (Part I), and Vol 49, No 5, May 1953, pp 226-234 (Part II).
13. Doumas, M., and Laster, R., "Liquid-Film Properties for Centrifugal Spray Nozzles," Chemical Engineering Progress, Vol. 49, No. 10, October 1953, pp 518-526.
14. Dumouchel, C, Bloor, M. I. G., Dombrowski, N., Ingham, D. B., and Ledoux, M., "Viscous Flow in a Swirl Atomizer," Chemical Engineering Science, Vol, 48, No 1, 1993, pp 81-87.
15. Yule, A. J., and Chinn, J. J., "Swirl Atomizer Row: Classical Inviscid Theory Revisited," International Conference on Liquid Atomization and Spray Systems (ICLASS-94), Rouen, France, July 1994
16. Dombrowski, N., and Hasson, D., "The Flow Characteristics of Swirl (Centrifugal) Spray Pressure Nozzles with Low Viscosity Liquids," AIChe Journal, Vol 15, No 4, July 1969, pp 604-611.
17. Simmons, H. C, "The Prediction of Sauter Mean Diameter for Gas Turbine Fuel Nozzles of Different Types," ASME Paper No. 79-WA/GT-5, Journal of Engineering for Power, 1979, pp 7.
18. Atherton, R. et al "Air Force Reusable Rocket Engine Program - Final Report," AFRPL-TR-71-1 Vol. 1 (Air Force Contract F04611-68-C-0002), Pratt & Whitney Aircraft, Division of United Aircraft Corp., January 1971.
19. Hautman, D. J., "Spray Characterization of Liquid/Gas and Liquid/Liquid Coaxial Injectors with the Center Liquid Swirled," Report No. UTRC89-31, United Technologies Research Center, East Hartford, CT., June 1990.
20. Hulka, J., Schneider, J. A., and Davis, J., "Single Element Injector Testing for STME Injector Technology," AIAA/SAE/ASME/ASEE 28th Joint Propulsion Conference and Exhibit, Nashville, TN., July 6-8, 1992.
21. Private communications with: G. Cox of Pratt & Whitney, J. Hulka of Aerojet Propulsion Division, and D. Hautmann of United Technologies Research Center.
22. Nurick, W. H., "Orifice Cavitation and its Effect on Spray Mixing," Journal of Fluids Engineering, Dec 1976, pp 681-687.
23. Van Dyke, M., Album of Fluid Motion, The Parabolic Press, Stanford, CA., 1982 ed, pp 115.
24. Farhangi, S., Hunt, K., Tuegel, L., Matthews, D., and Fisher, S., "Oxidizer-Rich Preburner for Advanced Rocket Engine Application," AIAA Paper 94-3260, AIAA/SAE/ASME/ASEE 30th Joint Propulsion Conference & Exhibit, Indianapolis, IN., June 27-29, 1994.