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S.N.B. Murthy, and E.T. Curran, High Speed Flight Propulsion Systems, Progress in Aeronautics and Astronautics, 1991, Vol. 137, AIAA, Inc., Washington DC.
M. Bulman and A. Siebenhaar, The Strutjet Engine: Exploding the Myths Surrounding High Speed Airbreathing Propulsion, AIAA Paper 1995, 2475.
D. Landrum, M. Thames, D. Parkinson, and S. Gautney, Investigations of the Rocket Induced Flow Field in a Rectangular Duct, AIAA Paper 1999, 2100.
D. Lineberry, N. Smith, D.B. Landrum, and C.W. Hawk, Characterization of Cold Flow Non-Axisymmetric Ejectors, AIAA Paper 2003, 5231.
D. Lineberry, Characterization of a Cold Flow Non-Axisymmetric Supersonic Ejector, Dissertation, Dept. of Mechanical and Aerospace Engineering, UAHuntsville, 2007.
H.W. Coleman, and W.G. Steele, Experimentation and Uncertainty Analysis for Engineers, Wiley-Interscience, 1999.
ESI Corporation, CFD Fastran Theory Manual, 2003.
D. Wilcox, Turbulence Modeling for CFD, DCW Industries Inc., Griffin Printing, CA, 1994.
B.S. Baldwin, and H. Lomax, Thin Layer Approximation and Algebraic Model for Separated Turbulent Flows, AIAA Paper 1978, 0257.
P.R. Spalart, and S.R. Allmaras, A One equation Model for Aerodynamic Flows, AIAA Paper 1992, 0439.
B.E. Launder, and D.E. Spalding, D. E., The Numerical Computation of Turbulent Flow, Comp. Methods App. Mech. Eng., 1974, 3, 269-289.
CrossRef
F.R. Menter, Zonal Two Equation Model for Aerodynamic Flows, AIAA Paper 1993, 2906.
F.R. Menter, F. R., Two Equation Eddy-viscosity Turbulence Models for Engineering Applications, AIAA Journal, 1994, 32, 1598-1606.
CrossRef
P.L. Roe, Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes, Journal of Computational Physics, 1981, 43(3), 57-372.
S.J. Osher, and S. Chakravarthy, Upwind Schemes and Boundary Conditions with Applications to Euler Equations in General Geometries, Journal of Computational Physics, 1983, 50, 447-81.
CrossRef
J. Fabri, and R. Siestrunck, Supersonic Air Ejectors, Advances in Applied Mechanics, Academic Press, NY, NY, 1958, 5, 1-34.
J. Fabri, and J. Paulon, Theory and Experiments on a Supersonic Air-To Air Ejectors, NACA Technical Memorandum, 1956, 1410.
K. Matsuo, Y. Miyazato, and H.D. Him, Shock Train and Pseudo-shock Phenomena in Internal Gas Flows, Prog. In Aserospace Science, 1999, 35, 33-100.
Y. Bartosiewicz, Z. Aidoun, P. Desevaux, and Y. Mercadier, Numerical and Experimental Investigations on Supersonic Ejectors," Int. J. Heat and Fluid Flow, 2005, 26, 56-70.
CrossRef
O. Zeman, Dilatational Dissipation: The Concept and Application in Modeling Compressible Mixing Layer, Physics of Fluids A, 1990, 2(2), 178-188.
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J.R. Viegas, and M.W. Rubesin, A Comparative Study of Several Compressibility Corrections to Turbulence Models Applied to High Speed Shear Layers, AIAA Paper 1991, 1783.
S. Sarkar, G. Erlebacher, M.Y. Hussaini, and H.O. Kreiss, The Analysis and Modeling of Dilatational Terms in Compressible Turbulence, J. Fluid Mech., 1991, 227, 473-493.
CrossRef
J.R. Forsythe, K.A. Hoffmann, and Y.B. Suzen, Investigation of Modified Menter's Two-Equation Turbulence Models for Supersonic Applications, AIAA Paper 1999, 0873.