Reduced-order modeling of two-dimensional supersonic flows with applications to scramjet inlets

Journal of Propulsion and Power

Volumn 26, Issue 3, 2010, Pages 545-555

  Dalle, Derek J ^a,b   Fotia, Matt L ^a,b   Driscoll, James F ^a,b  

^a UNIVERSITY OF MICHIGAN   (United States)

^b Department of Aerospace Engineering ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; COMPUTATIONAL FLUID DYNAMICS; HYPERSONIC FLOW; HYPERSONIC VEHICLES; PROPULSION; RAMJET ENGINES; SUPERSONIC AIRCRAFT; SUPERSONIC FLOW;

BLUNT LEADING EDGES; COMPUTATIONAL TIME; CONTROL ORIENTED MODELS; DISPLACEMENT THICKNESS; MULTIPLE WAVE INTERACTION; REDUCED ORDER MODELS; TWO-DIMENSIONAL GEOMETRY; VEHICLE PROPULSION SYSTEMS;

HYPERSONIC INLETS;

EID: 77952559244     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/1.46521     Document Type: Article

References (13)

1. Bogar, T. J., Alberico, J. F., Johnson, D. B., Espinosa, A. M., and Lockwood, M. K., "Dual-Fuel Lifting Body Configuration Development," AIAA Paper 96-4592, 1996.
2. 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. doi:10.2514/1.23370 (Pubitemid 46741383)
3. Brown, M., Mudford, N. R., Neely, A. J., and Ray, T., "Robust Optimization of Two-Dimensional Scramjet Inlets," AIAA Paper 2006-8140, 2006.
4. Chavez, F. R., and Schmidt, D. K., "Analytical Aeropropulsive/ Aeroelastic Hypersonic-Vehicle Model with Dynamic Analysis," Journal of Guidance, Control, and Dynamics, Vol.17, No.6, 1994, pp. 1308-1319. doi:10.2514/3.21349
5. Smart, M. K., "Optimization of Two-Dimensional Scramjet Inlets," Journal of Aircraft, Vol.36, No.2, 1999, pp. 430-433. doi:10.2514/2.2448
6. Billig, F. S., "Shock-Wave Shapes Around Spherical-and Cylindrical-Nosed Bodies," Journal of Spacecraft and Rockets, Vol.4, 1967, pp. 822-823. doi:10.2514/3.28969
7. Emanuel, G., Analytical Fluid Dynamics, CRC Press, Boca Raton, FL, 2001, Chap. 9.
8. Ismail, M., "Prandtl-Meyer Flow of a Calorically Imperfect Gas," Master's Thesis, School of Aerospace and Mechanical Engineering, Univ. of Oklahoma, Norman, OK, 1994.
9. Zebbiche, T., "Stagnation Temperature Effect on the Prandtl-Meyer Function," AIAA Journal, Vol.45, No.4, 2007, pp. 952-954. doi:10.2514/1.24868 (Pubitemid 46643609)
10. Tatum, K. E., "Computation of Thermally Perfect Oblique Shock Wave Properties," AIAA Paper 1997-868, 1997.
11. Anderson, J. D., Fundamentals of Aerodynamics, 2nd ed., McGraw-Hill, New York, 1991.
12. White, F. M., Viscous Fluid Flow, 3rd ed., McGraw-Hill, New York, 2006.
13. Emami, S., Trexler, C. A., Auslender, A. H., and Weidner, J. P., "Experimental Investigation of Inlet-Combustor Isolators for a Dual-Mode Scramjet at a Mach Number of 4," NASATechnical Paper 3502, May 1995.