Nozzle performance predictions using the TDK 97 code

33rd Joint Propulsion Conference and Exhibit

Volumn , Issue , 1997, Pages

  Dunn, Stuart S ^a   Coats, Douglas E ^a  

^a Software and Engineering Associates Inc   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE VEHICLES; BOUNDARY LAYERS; CODES (SYMBOLS); ENGINES; GAS GENERATORS; NOZZLES; NUMERICAL METHODS; PROPULSION; RADIATION EFFECTS; ROCKETS; SURFACE ROUGHNESS; TRANSPIRATION;

FINITE-RATE CHEMISTRY; HETEROGENEOUS REACTIONS; LAMINAR TURBULENT TRANSITIONS; METHOD OF CHARACTERISTICS; ORBIT TRANSFER VEHICLES; PERFORMANCE PREDICTION; SPACE TRANSPORTATIONS; TRANSPIRATION COOLING;

DUAL FUEL ENGINES;

EID: 84962799491     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (16)

1. Pieper, J.L., "ICRPG Liquid Propellant Thrust Chamber Performance Evaluation Manual", CPIA 178, Sept. 1968.
2. "JANNAF Rocket Engine Performance Prediction and Evaluation," CPIA 246, April 1975.
3. Sutton, G.P. Rocket Propulsion Elements Sixth Edition, John Wiley & Sons, Inc. New York, 1992.
4. Zucrow, M.J. and Hoffman, J.D. Gas Dynamic, John Wiley & Sons, Inc. New York, 1976.
5. Gordon, S. and McBride, B.J., "Computer Program for Calculation of Complex Chemical Equilibrium Compositions, Rocket Performance, Incident and Reflected Shocks, and Chapman Jouguet Detonations," NASA SP 273, 1971.
6. Gordon, S. and McBride, B.J., "Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications," NASA RP 131 1, Oct. 1994.
7. Nickerson, G.R., Berker, D.R., Coats, D.E., and Dunn, S.S., ’Two-Dimensional Kinetics (TDK) Nozzle Performance Computer Program Volume 11, Users Manual", prepared by Software and Engineering Associates, Inc. for George C. Marshall Space Flight Center under contract NAS8-39048, March 1993.
8. Cebeci, T. and Smith, A.M.O., Analysis of Turbulent Boundary Layers, Academic Press, N. Y., 1974.
9. Levine, J.N., "Transpiration and Film Cooling Boundary Layer Computer Program", Dynamic Science, prepared for NASA, contract NAS7i- 791, June 1971.
10. Sauer, R., "General Characteristics of the Flow Through Nozzles at Near Critical Speeds", NACA Tech. Note No. 1147 (1947).
11. Nickerson, G.R. "Striated Flow in a Converging- Diverging Nozzle", Dynamic Science Report CS- 217 1- 1, prepared for NASA JSC, February 1971.
12. Kushida, R., "Revision of CPIA 246, Section 6.2, Reaction Rate Data," JPL 383CR-76-21 1, March 1976.
13. Coats, D.E., Berker, D.R., and Kawasaki, A.H., "Boundary Layer Loss Models In Nozzle Performance Predictions," 26th JANNAF Combustion Meeting, JPL, Pasadena, CA, Oct. 1989. 14.
14. Kehtarnavaz, H., Coats, D.E., and Dang, A.L., "Viscous Loss Assessment in Rocket Engines", Journal of Propulsion and Power, Vol. 6,No. 6, pp 713-717, Nov.-Dec., 1990.
15. Kushida, R., Hermal, J., Apfel, S., and Zydowicy, M., "Performance of High-Area Ratio Nozzle for a Small Rocker Thruster," Journal of Propulsion and Power, Vol. 3, No. 4, pg 329.
16. Kliegel, J.R., Nickerson, G.R., Frey, H.M., Quan, V., and Melde, J.E., "Two-Dimensional Kinetics Nozzle Analysis Computer Program- TDK", Prepared for the ICRPG Performance Standardization Working Group, July 1968.