Study on design- and operation- parameters of supersonic exhaust diffusers

46th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2008, Pages

  Sung, Honggye ^a   Yoon, Sangkyu ^a   Yeom, Hyowon ^a   Kim, Jinkon ^a   Ko, Yongsung ^b   Kim, Yongwook ^c   Oh, Seunghyup ^c  

^a Hankuk Aviation University   (South Korea)

^b Chungnam National University   (South Korea)

^c Korea Aerospace Research Institute (KARI)   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

AREA RATIOS; AXISYMMETRIC CONFIGURATIONS; EXPERIMENTAL APPROACHES; HIGH ALTITUDE; NITROGEN GAS; OPERATION CHARACTERISTIC; PHYSICAL MODEL; PHYSICAL PHENOMENA; ROCKET MOTOR; STARTING PRESSURE; SUPERSONIC EXHAUST DIFFUSERS; VACUUM CHAMBERS;

AEROSPACE ENGINEERING; NITROGEN; ROCKET ENGINES; ROCKET NOZZLES; ROCKETS; VACUUM;

NOZZLE DESIGN;

EID: 78149420269     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)

1. Sivo, J.N., Meyer, C.L. and Peters, D.J., "Experimental Evaluation of Rocket Exhaust Diffusers for Altitude Simulation," NASA-TN-D-298, 1960.
2. Goethert, B.H., "High Altitude and Space Simulation Testing," ARS Journal, 1962, pp872-882.
3. Massier, P.F. and Roschke, E.J., "Experimental Investigation of Exhaust Diffusers for Rocket Engines," JPL-TR-32-210, 1962.
4. German, R.C., Bauer, R.C. and Panesci, J.H., "Methods for Determining the Performance of Ejector-Diffuser Systems," Journal of Spacecraft and Rockets, Vol. 3, No. 2, 1966, pp. 193-200.
5. Wojciechowski, C.J. and Anderson, P.G., "Parametric Analysis of Diffuser Requirements for High Expansion Ratio Space Engine," LMSC-HREC-TR-D784489, NASA-CR-161924, 1981.
6. McAmis, R. and Bartlett, C., "Aerodynamic Free-Jet Nozzle Performance Augmentation Using An Exhaust Diffuser," AIAA Paper 91-2270, 27th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Sacramento, CA, 1991.
7. Stephens, S.E., "Experimental and Computational Data from a Small Rocket Exhaust Diffuser," AIAA Paper 93-1860, 29th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Monterey, CA, 1993.
8. Annamalai, K., Visvanathan, K., Sriramulu, V., Bhaskaran, K.A., "Evaluation of the performance of supersonic exhaust diffuser using scaled down models," Experimental Thermal and Fluid Science, Vol. 17, Issue 3, July, 1998, pp.217-229.
9. Quebert, L. and Garcia, Y., "Theoretical and Experimental Design of an Exhaust Diffuser for an Upper Stage Engine of a Ballistic Missle," AIAA Paper 2001-3382, 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Salt Lake City, Utah, 2001.
10. Otterstatter, M.R., Meyer, S.E., Heister, S.D., Dambach, E.M., "Design of an Altitude-testing Facility for Lab-Scale Propulsion Devices," AIAA Paper 2007-5323, 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Cincinnati, OH, 2007.
11. Yang, Z. and Shih, T. H., "New Time Scale Based κ -ε Model for Near-Wall Turbulence," AIAA Journal, Vol. 31, No. 7, 1993, pp. 1191-1197.