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Inlet & Nozzle Branch
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Inlet and Nozzle Branch Key Publications

Abbott, John M.: Computational Study of the Aerodynamic Performance of Subsonic Scarf Inlets. AIAA-2004-3406, 2004.

Bush, R. H., Power, G. D., and Towne, C. E., "WIND: The Production Flow Solver of the NPARC Alliance," AIAA Paper 98-0935

Cavicchi, Richard H.: "A Three-Dimensional CFD Investigation of Secondary Flow in an Accelerating, 90 Degree Elbow". NASA TM- 2001-211219, December 2001.

Cavicchi, Richard H.: "Probing Within the Boundary Layer of an Airfoil by Using the WIND Numerical Code", NASA TM-2004-213221, September 2004.

CGNS Project Group, CFD General Notation System

Chima. R. V., "A Three-Dimensional Unsteady CFD Model of Compressor Stability," ASME Paper GT2006-90040, May 2006. Also NASA TM-2006-214117.

Chima., R. V. and Liou, M.-S., "Comparison of the AUSM+ and H-Cusp Schemes for Turbomachinery Applications," AIAA Paper AIAA-2003-4120, June 2003. Also NASA TM-2003-212457.

Chima, R. V., "Calculation of Multistage Turbomachinery Using Steady Characteristic Boundary Conditions," AIAA Paper 98-0968, Jan. 1998. Also NASA TM-1998-206613.

Chima, R. V., "Viscous Three-Dimensional Calculations of Transonic Fan Performance," in CFD Techniques for Propulsion Applications, AGARD Conference Proceedings No. CP-510, AGARD, Neuilly-Sur-Seine, France, Feb. 1992, pp 21-1 to 21-19. Also NASA TM-103800.

Conley (Dudek), J. M., Leonard, B. P., "Modification of the MML turbulence model for adverse pressure gradient flows," AIAA Paper No. AIAA-1994-2715, June, 1994.

Dalbello, T., Dippold, V., Georgiadis, N., “Computational Study of Separating Flow in a Planar Subsonic Diffuser,” NASA/TM-2005-213894, October 2005.

DeBonis, J.R., “Progress Towards Large-Eddy Simulations for Prediction of Realistic Nozzle Systems,” AIAA Paper 2006-0487, January 2006.

DeBonis, J.R. and Scott, J.N., “A Large-Eddy Simulation of a Turbulent Compressible Round Jet,” AIAA Journal, Vol. 40, No. 7, pp. 1346-1354, July 2002.

DeBonis, J.R., Steffen Jr., C.J., Rice, T., and Trefny, C.J., “Design Evolution and Performance Characterization of the GTX Air-Breathing Launch Vehicle Inlet,” Proceedings of the JANNAF 26th Airbreathing Propulsion Subcommittee Meeting, Destin, FL, April, 2002.

DeBonis, J.R. and Scott, J.N., “A Study of the Error and Efficiency of Numerical Schemes for Computational Aeroacoustics,” AIAA Journal, Vol. 40, No. 2, pp. 227-234, February 2002.

DeBonis, J.R., “Analysis and Parametric Study of a Mixer/Ejector Nozzle for Application to the High Speed Civil Transport,” NASA TM 2000-210038, April 2000.

Dippold, V. F., Hosder, S., Schetz, J. A., “Analysis of Jet-Wing Distributed Propulsion From Thick Wing Trailing Edges,” 42nd AIAA Aerospace Sciences Meeting & Exhibit, AIAA 2004-1205, January 5-8, 2004.

Dippold, V. F., “Investigation of Wall Function and Turbulence Model Performance within the Wind Code,” 43rd AIAA Aerospace Sciences Meeting & Exhibit, AIAA 2005-1002, January 10-13, 2005.

Dippold, V., Mohler, S., “Validation of Wind-US Unstructured Flow Solver for Wall-Bounded Flows,” 44th AIAA Aerospace Sciences Meeting & Exhibit, AIAA-2006-0637, January 9-12, 2006.

Dudek, J. C., "An Empirical Model for Vane-Type Vortex Generators in a Navier-Stokes Code," AIAA Paper no. 2005-1003, January, 2005.

Dudek, J. C., Georgiadis, N. J., and Yoder D. A., (Cincinnati, Univ., OH), "Calculation of turbulent subsonic diffuser flows using the NPARC Navier-Stokes code," AIAA Paper no. AIAA-1996-497 V, January, 1996.

Fernandez, R.; and Nenni, J. P., "Pulsed Detonation Engine Inlet Experimental And CFD Results", TM-2002-211581, JANNAF APS 04/2002.

Fernandez, R.; Slater, J. W.; and Paxson, D. E., "NASA´s Pulsed Ejector Wave Propagation Test Program" International Colloquium on Advances in Confined Detonations, Moscow, Russia, 07/02/2002.

Fernandez, R.; Slater, J. W.; and Paxson, D. E., "NASA Glenn´s Pulsed Ejector Wave Propagation Test Program" in book "Confined Detonations & Pulse Detonation Engines" pp. 311-334, Torus Press Publ., Moscow, ISBN 5-94588-012-4, 2003.

Georgiadis, N.J., Alexander, J.I.D., and Reshotko, E., "Hybrid Reynolds-Averaged Navier-Stokes/Large-Eddy Simulations of Supersonic Turbulent Mixing," AIAA Journal, Vol. 41, No. 2, Feb. 2003, pp. 218-229.

Georgiadis, N.J. and Papamoschou, D., "Computations of Dual-Stream Jets with Eccentric and Coaxial Bypass Streams," AIAA Paper 2004-2981, May 2004.

Georgiadis, N.J., DalBello, T.W, Trefny, C.J., and Johns, A.L., "Aerodynamic Design and Analysis of High Performance Nozzles for Mach 4 Accelerator Vehicles, AIAA Paper 2006-0016, Jan. 2006.

Georgiadis, N.J., Yoder, D.A., and Engblom, W.A., "Evaluation of Modified Two-Equation Turbulence Models for Jet Flow Predictions, AIAA Paper 2006-0490, Jan. 2006 and accepted for publication in the AIAA Journal.

Georgiadis, N.J., Rumsey, C.L., Yoder, D.A., and Zaman, K.B.M.Q., "Turbulence Modeling Effects on Calculation of Lobed Nozzle Flowfields," J. Propulsion and Power, Vol. 22, No. 3, May 2006, pp. 567-575.

Greber, I.; and Fernandez, R., "Molecular Dynamics Simulation of Unsteady Diffusion", APS Division of Fluid Dynamics, (Abstract and Oral) 11/2002.

Kim, Hyun D.; and Saunders, John D.: Embedded Wing Propulsion Conceptual Study. In Vehicle Propulsion Integration Symposium, Warsaw, Poland, Oct. 2003, NASA/TM-2003-212696, November, 2003.

Legensky, S. M., Edwards, D. E., Bush, R. H., Poirier, D. M. A., Rumsey, C. L., Cosner, R. R., and Towne, C. E., "CFD General Notation System (CGNS): Status and Future Directions" AIAA Paper 2002-0752.

Milanovic, I.M. and Zaman, K.B.M.Q., 2005, "Synthetic Jets in Crossflow", AIAA J., 43(5), pp. 929-940.

Mizukami, Masashi; and Saunders, John: Parametrics on 2D Navier-Stokes Analysis of a Mach 2.68 Bifurcated Rectangular Mixed-Compression Inlet. AIAA paper #95-2755, 31st Joint Propulsion Conference, July 10-12 1995. NASA TM-107003.

Mizukami, Masashi; and Saunders, John: 3D Navier-Stokes Analysis of a Mach 2.68 Bifurcated Rectangular Mixed-Compression Inlet. AIAA paper #96-0495, 34th Aero. Sciences Mtg, January 15-18 1996. NASA TM-107123.

Nori, V.; Lerma, N.; Gustavsson, J.; Segal, C.; and Fernandez, R. “Forced Oscillations in a Mixed-Compression Inlet at Mach 3.5 for Pulse Detonation Engine Systems”, ASME Journal of Fluids Engineering, Vol. 128, May 2006.

NPARC Alliance, Wind-US Documentation

Saunders, John D.; Frate, Franco C.; and Wendt, Bruce J.: Inlet Design Methods for an X43B Demonstrator. 27th Airbreating Propulsion Subcommittee meeting, December 2003.

Saunders, John D.; and Keith, Theo G.: Results from Computational Analysis of a Mixed Compression Supersonic Inlet. NASA TM-104475, (AIAA #91-2581), Joint Propulsion Conference, June 24-26 1991.

Slater, J.W., D.O. Davis, B.W. Sanders, and L.J. Weir, “Role of CFD in the Aerodynamic Design and Analysis of the Parametric Inlet,” ISABE-2005-1168, September 2005.

Slater, J.W. and C.R. Gruber, “Planar Inlet Design and Analysis Process (PINDAP)”, AIAA Paper 2005-4203, July 2005. Also NASA TM-2005-213866.

Slater, J.W. and G.E. Welch, “Design of a Wave Rotor Transition Duct,” AIAA Paper 2005-5143, June 2005.

Slater, J.W., “CFD Methods for Computing the Performance of Supersonic Inlets,” AIAA Paper 2004-3404, July 2004.

Slater, J.W., J.M. Abbott, and R.H. Cavicchi, “Validation of WIND for a Series of Inlet Flows”, AIAA Paper 2002-0669, January 2002. Also NASA TM-2002-211907.

Slater, J.W., “Verification Assessment of Flow Boundary Conditions for CFD Analysis of Supersonic Inlet Flows”, AIAA Paper 2001-3882, July 2001.

Slater, J.W. and G.C. Paynter, “Implementation of a Compressor Face Boundary Condition Based on Small Disturbances,” ASME Journal of Turbomachinery, Vol. 123., April 2001. Also NASA TM 2000-209945.

Slater, J.W., J.C. Dudek, and K.E. Tatum, “The NPARC Verification and Validation Archive”, ASME Paper 2000-FED-11233, June 2000. Also NASA TM-2000-209946.

Tacina, K.M., Fernandez, R., and Moody, S.M., "Thrust Augmentation in an Unsteady Supersonic Ejector", AIAA 2004-0866, 2004.

Tacina, K.M., Fernandez, R., Slater, J.W., and Moody, S.M., "An Analysis of Pitot and Static Pressure Measurements in an Unsteady Supersonic Flow," AIAA 2004-2719.

Thomas, Scott R.; Saunders, John D.; Walker, James F.; and Capriotti, Diego P.: Mach 3.5 to 7 Free-Jet Engine Tests of the GTX RBCC Flowpath with a 12 deg.-Spike Inlet. Presented at the 2000 JANNAF Propulsion and Joint Subcommittee Meetings, Monterey, CA, November 13-17, 2000.

Towne, C. E., "Inlet, Duct, and Nozzle Flows," in "Applied Computational Fluid Dynamics", Garg, V. K., ed., Marcel Dekker, Inc., New York, 1998.

Wendt, B. J., and Dudek, J. C., "Development of Vortex Generator Use for a Transition High-Speed Inlet," Journal of Aircraft, Vol. 35, No. 4, July 1988.

Yoder, D.A., Georgiadis, N.J., and Wolter, J.D., "Quadrant CFD Analysis of a Mixer-Ejector Nozzle for HSCT Applications," NASA TM 2005-213602, April 2005.

Yoder, D.A., "Initial Evaluation of an Algebraic Reynolds Stress Model for Compressible Turbulent Shear Flows," AIAA-2003-0548, Jan. 2003.

Yoder, D.A., and Georgiadis, N.J., "Implementation and Validation of the Chien k-epsilon Turbulence Model in the WIND Navier-Stokes Code," AIAA 99-0745/NASA TM 1999-209080, Jan. 1999.

Yoder, D.A., Georgiadis, N.J., and Orkwis, P.D., "Implementation of a Two-Equation k-omega Turbulence Model in NPARC," AIAA 96-0383/NASA TM 107080, Jan. 1996.

Zaman, K.B.M.Q., 1998, "Asymptotic spreading rate of initially compressible jets experiment and analysis", Physics of Fluids, 10, pp. 2652-2660.

Zaman, K.B.M.Q., 1999, "Spreading characteristics of compressible jets from nozzles of various geometries", J. Fluid Mech., 383, pp. 197-228.

Zaman, K.B.M.Q., Dahl, M.D., Bencic, T.J. and Loh, C.Y., 2002, "Investigation of a 'transonic resonance' with convergent-divergent nozzles", J. Fluid Mech., 463, pp. 313-343.

Zaman, K.B.M.Q., Wang, F.Y. and Georgiadis, N.J., 2003, "Noise, turbulence and thrust of subsonic free jets from lobed nozzles", AIAA J., 41(3), pp. 398-407.


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Last Updated: Tuesday, 13-Jan-2009 13:54:41 EST