A scramjet engine model including effects of precombustion shocks and dissociation

44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2008, Pages

  Torrez, Sean M ^a   Scholten, Nathan A ^a   Micka, Daniel J ^a   Driscoll, James F ^a   Bolender, Michael A ^b   Doman, David B ^b   Oppenheimer, Michael W ^b  

^a UNIVERSITY OF MICHIGAN   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AUTO-IGNITION; COMBUSTION PRO-CESS; DYNAMICS AND CONTROL; FINITE-RATE CHEMISTRY; FLOW PHYSICS; FUEL-AIR MIXING; GAS DISSOCIATION; GOVERNING EQUATIONS; HYPERSONIC FLIGHTS; NEW MODEL; PRE-COMBUSTIONS; PROPULSION MODELS; PROPULSION SYSTEM; RAYLEIGH FLOW; REACTION MECHANISM; REDUCED ORDER MODELS; SCRAMJET ENGINES; SHOCK TRAIN; STAGNATION PRESSURES; SUBMODELS; SYSTEM ANALYSIS; TIME-SCALES; VEHICLE AERODYNAMICS; VEHICLE DESIGN; WALL HEAT TRANSFER;

AUTOMOBILE ENGINES; AUTOMOBILE PARTS AND EQUIPMENT; COMBUSTION; CONTROL SYSTEM ANALYSIS; DISSOCIATION; FLIGHT CONTROL SYSTEMS; FLIGHT ENVELOPES; FRICTION; HYPERSONIC AERODYNAMICS; HYPERSONIC VEHICLES; MACH NUMBER; PROPULSION; STRUCTURAL DYNAMICS;

COMPUTER SIMULATION;

EID: 77957852506     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (39)

1. Bolender, M. A. and Doman, D. B., "Nonlinear Longitudinal Dynamical Model of an Air-Breathing Hypersonic Vehicle," Journal of Spacecraft and Rockets, Vol. 44, No. 2, 2007, pp. 374-387.
2. Oppenheimer, M.W. and Doman, D. B., "A Hypersonic Vehicle Model Developed with Piston Theory" AIAA 2006-6637, 2006.
3. Oppenheimer, M. W., Doman, D. B., Bolender, M. A., and Skujins, T., "A Flexible Hypersonic Vehicle Model Developed with Piston Theory," AIAA Paper 2007-6396, 2007.
4. Oppenheimer, M. W. and Doman, D. B., "Viscous Effects for A Hypersonic Vehicle Model," In preparation for submittal to the 2008 AIAA Atmospheric Flight Mechanics Conference.
5. Williams, T., Bolender, M. A., Doman, D. B., and Morataya, O., "An Aerothermal Flexible Mode Analysis of a Hypersonic Vehicle," AIAA Paper 2006-6647, 2006.
6. Bolender, M.A. and Doman, D.B., "Nonlinear Longitudinal Dynamical Model of an Air-Breathing Hypersonic Vehicle", J. Spacecraft and Rockets Vol. 44, No. 2, 2007, pp. 374-387.
7. Chavez, F.R. and Schmidt, D.K., "Analytical Aeropropulsive/ Aeroelastic Hypersonic Vehicle Model", J. Guidance, Control, Dynamics Vol.17, No. 6, 1994, pp.1308-1317.
8. Tarpley, C. and Lewis, M.J., "Stability Derivatives for a Hypersonic Caret Wing Waverider", J. Aircraft Vol. 32, No. 4, 1995, pp.795-801.
9. Shapiro, A.H., Dynamics and Thermodynamics of Compressible Fluid Flow, Ronald Press NY, 1953.
10. O'Brien, T.F., Starkey, R.P., Lewis, M.J., "Quasi-One-Dimensional High-Speed Engine Model with Finite-Rate Chemistry". J. Propulsion and Power Vol. 17, No. 6, 2001, pp. 1366-1374.
11. Starkey, R.P., "Off-Design Performance Characterization of a Variable Geometry Scramjet", AIAA Paper 2005-3711, 2005.
12. Birzer, C., Doolan, C.J., "Quasi-One-Dimensional Modeling of Hydrogen Fuelled Scramjet Combustors". AIAA Paper 2007-4314, 2007.
13. Tetlow, M.R., Doolan, C.J., "Comparison of Hydrogen and Hydrocarbon-Fueled Scramjet Engines for Orbital Insertion", J. Spacecraft and Rockets Vol. 44, No. 2, 2007, pp. 365-372.
14. Zambon, A.C. and Chelliah, H.K., "Explicit Reduced Reaction Models for Ignition, Flame Propagation, and Extinction of C2H4/CH4/H2 and Air Systems", Combustion and Flame Vol. 150, 2007, pp. 71-91.
15. Heiser, W.H. and Pratt, D.T., Hypersonic Airbreathing Propulsion, AIAA Education Series, AIAA Pub., Washington DC, 1994.
16. Anderson, Jr., J.D., Hypersonics and High Temperature Gas Dynamics, McGraw-Hill Pub. NY, 1989.
17. Hasselbrink, E.F. and Mungal, M.G., "Transverse Jets and Jet Flames: Part 1. Scaling Laws for Strong Transverse Jets", J. Fluid Mech. Vol. 443, 2001, pp.1-25.
18. Smith, S.H. and Mungal, M.G., "Mixing, Structure and Scaling of the Jet in Crossflow", J. Fluid Mech. 357, 1998, pp. 83-122.
19. Kuo, K.K., Principles of Combustion, Wiley and Sons Pub, NY, 2005.
20. Broadwell, J.E. and Breidenthal, R.E., "Structure and Mixing of a Transverse Jet in Incompressible Flow", J. Fluid Mech. Vol. 148, 1984, pp. 405-412.
21. Huang, R.F. and Chang, J.M., "The Stability and Visualized Flame and Flow Structures of a Combusting Jet in Cross Flow". Combust. Flame Vol. 98, 1994, pp. 267-278.
22. Kalghatgi, G.T., "The Visible Shape and Size of a Turbulent Hydrocarbon Jet Diffusion Flame in a Cross-wind", Combust. Flame, Vol. 52, 1983, pp. 91-106.
23. Majeski, A.J., Wilson, D.J., Kostiuk, L.W., "Predicting the Length of Low-momentum Jet Diffusion Flames in Crossflow", Combustion Science and Technology Vol. 176, No. 12, 2004, pp. 2001-2025.
24. Kostiuk, L.W., Majeski, A.J., Poudenx, P., "Scaling of Wake-stabilized Jet Diffusion Flames in a Transverse Air Stream", Proceedings of the Combustion Institute Vol. 28, 2000, pp. 553-559.
25. Gruber, M.R., Nejad, A.S., Chen, T.S., Dutton, J.C., " Compressibility Effects in Supersonic Transverse Injection Flowfields", Phys. Fluids Vol. 9, No. 5, 1997, pp. 1448-1455.
26. Heister, S.D. and Karagozian, A.R., "Gaseous Jets in Supersonic Crossflow", AIAA J. Vol. 28, 1990, pp. 819-827.
27. Driscoll. J.F., Huh, H., Yoon, Y., Donbar, J., "Measured Lengths of Supersonic Hydrogen Air Jet Flames - Compared to Subsonic Flame Lengths and Analysis", Combust. Flame Vol. 107, 1996, pp. 176-186.
28. Heiser, W.H. and Pratt, D.T., Progress in Aeronautics and Astronautics, Vol. 189, 2001, pp. 569-581.
29. Billig, F.S., "Research on Supersonic Combustion", J. Propulsion and Power, Vol. 9, No. 4, 1993, pp. 499-504.
30. Billig, F.S., "Combustion Processes in Supersonic Flow", J. Propulsion and Power, Vol. 4, No. 3, 1988, pp. 209-224.
31. Billig, F.S. and Dugger, G.L., "Predictions of Precombustion Wall Pressure Distributions in Scramjet Engines", J. Spacecraft and Rockets, Vol. 10, No. 9, 1973, pp. 620-622.
32. Billig, F.S. and Dugger, G.L., "The Interaction of Shock Waves and Heat Addition in the Design of Supersonic Combustors", Proc. Combust. Inst. Vol. 12, 1969, pp. 1125-1132.
33. Billig, F.S., "Proposed Supplement to Propulsion System Management Support Plan", JHU/APL report July 15, 1986.
34. Baurle, R.A. and Eklund, D.R., "Analysis of Dual-Mode Hydrocarbon Scramjet", J. Propulsion and Power Vol.18, No. 5, 2002, pp. 990-1002.
35. Tam, C.J., Baurle, R.A., Gruber, M.R., "Numerical Study of Jet Injection into a Supersonic Crossflow", AIAA Paper 99-2254, 1999.
36. Sullins, G.A., "Demonstration of Mode Transition in a Scramjet Combustor", J. Propulsion and Power Vol. 9, No. 4, 1993, pp. 515-521.
37. Dessornes, O., "Tests of the JAPHAR Dual Mode Ramjet Engine", Aerospace Science and Techol. Vol. 9, 2005, pp. 211-219.
38. Tam, C.J., Eklund, D., Behdadnia, R. and Jackson, T., "Investigation of Boundary Layer Bleed for Improving Scramjet Isolator Performance", AIAA Paper 2005-3286, 2005.
39. Nedungadi, A. and Van Wie, D.M., "Understanding Isolator Performance Operating in the Separated Shock Mode", AIAA Paper 2004-3832, 2004.