A Partial List of
ANSWER™ PUBLICATIONS

Important note: This partial list is provided as an informative collection only. ACRi does not have electronic or hard copies of these publications, and legally cannot re-distribute copyrighted material. If you would like to have a copy of a certain paper/book, please contact either the authors or the respective publisher directly. Inquiries on this matter will not be addressed by ACRi.

D.B. Schein and W.C. Meecham, 2001. Computation of Jet Noise at Realistic Mach and Reynolds Numbers Using Large-Eddy Simulation and Lighthill's Analogy. FEDSM2001-18144, ASME 2001 Fluids Eng. Division Summer Meeting, May 29-June 1, New Orleans, LA.

G.N. Kumar and H. Mongia, 2000. Results Of A DOE On the Film Cooling Effectiveness Of a Modern Combustor with Machined Ring Liners. AIAA-2000-2235, 36th AIAA/ASME/ASEE Joint Propulsion Conference, July 2000, Huntsville, AL

G.N. Kumar and H.C. Mongia, 2000 Assessment Of Advanced Turbulence Models And Unstructured Code For Calculating The Film Effectiveness Of A Modern Film-Cooled Combustor. AIAA-2000-0333, AIAA 38^th Aerospace Sciences Meeting, January 10-13, Reno, NV.

G.N. Kumar and H.C. Mongia, 2000. Validation Of Near Wall Turbulence Models For Film Cooling Applications In Combustors. AIAA-2000-0480, AIAA 38^th Aerospace Sciences Meeting, January 10-13, Reno, NV.

A.K. Runchal and M.M. Rao, 2000. Dynamically Programmable and User Friendly CFD Software for Industrial Applications. Invited Lecture - Intn'l Sym. on Challenges and New Directions in Computation of Internal Flows, IIT Madras, Chennai, Jan 7-8.

V. Sundararajan, 2000. CFD Experiences in Aero Engine Development. Invited Lecture . Intn'l Sym. on Challenges and New Directions in Computation of Internal Flows, IIT Madras, Chennai, Jan 7-8.

Grant Swenson, 1999. Numerical Simulations of Combustion Instabilities in Gas Turbine Combustors with Applications. Ph.D.Thesis, California Institute of Technology, Pasadena, CA.

G.N. Kumar and H. Mongia, 1999 Validation of Turbulence Models for Wall Jet Computations as Applied to Combustor Liners. AIAA-99-2250, 35^th AIAA/ASME/ASEE Joint Propulsion Conference, Los Angeles, California, June 20-24, 1999.

D.B. Schien and W.C. Meecham, 1999. Hot Jet Noise Computed from Time-Accurate Simulation of Compressible Free Jet Turbulence. Sixth International Congress on Sound and Vibration, July,1999, Copenhagen, Denmark

S. Lee, A.K. Runchal and J-O Han, 1999. Subgrid-Scale Modeling in Large-Eddy Simulation and its Application to Flow about Yawed Cylinder and Cavity Flows. 3^rd ASME/JSME FED Conf., Washington, D.C.

S. Lee, J-S Choi, J-O Han and A.K. Runchal, 1999. A Large-Eddy Simulation of the Turbulent Flow in the Vicinity of an Upright Wall-Mounted Half Cyliner and Aerodynamic Sound Prediction. 3^rd ASME/JSME Joint FED Conf., Washington, D.C.

H.C. Mongia, 1998. Aero-Thermal Design and Analysis of Gas Turbine Combustion Systems: Current Status and Future Direction.Paper # AIAA 98-3982, 34^th AIAA/ASME/SAE/ASEE, Propulsion Meeting, July 13-15, 1998, Cleveland, OH.

T.J. Held and H.C. Mongia, 1998. Emissions Modeling of Gas Turbine Combustors using a Partially-Premixed Laminar Flamelet Model. Paper# AIAA 98-3950, 34^th AIAA Propulsion Meeting, July 13-15, 1998, Cleveland, OH.

T.J. Held and H.C. Mongia, 1998 "Application of a Partially Premixed Laminar Flamelet Model to a Low Emissions Gas Turbine Combustor," ASME Paper No. 98-GT-217, Intern'l Gas Turbine & Aeroengine Congress.

T.J. Held and H.C. Mongia, 1998 "Emissions Modeling of Gas Turbine Combustors Using a Partially-Premixed Laminar Flamelet Model," AIAA Paper No. 98-3950

Robert Goler, 1998 Effect of Temperature Gradients on Flow Around a Building. M.S. Thesis, The Univ. of Adelaide, Dept of Applied Math., Adelaide, Australia.

D.B. Schein, 1998 Exhaust mixing noise computed from time-accurate simulation of compressible free jet turbulence. Paper 3pEA3, 136^th Meeting, Acoustical Society of America, Norfolk, Virginia.

S. Lee, 1998. Numerical Study of Aerodynamic Noise from a Rotating Cylinder Using Large-Eddy Simulation. 2^nd Year Report to KOSEF.

John S. Lang, 1998. Formulating Design Criteria for Hydraulic jet Mixing by Modeling. J. American Water Works Association. To be published.

D.B. Schein, 1997. Large-eddy simulation of compressible free jet turbulence applied to computation of exhaust mixing noise. Paper 4pNS3; 134^th Meeting, Acoustical Society of America, San Diego, CA.

D. B. Schein and W.C. Meecham, 1997. Computation of Jet Noise Using Large-Eddy Simulation and Lighthill's Analogy. ASME 4^th Intn'l Sym. on Fluid-Structure Interaction, Aeroelasticity, Flow-Induced Vibration and Noise, AD-Vol. 53-1. 439-446. IMECE, Dallas, Texas

S. Lee and W.C. Meecham, 1996. Computation of Noise from Homogeneous Turbulence and from a Free Jet. Int. J. Acoustics & Vibration, 1, 1, 35-47.

S. Lee, 1993. Computation of Aerosound from Turbulent Flow Fields Using Large-Eddy Simulation Proc. Noise '93 Conference p. 619-624, 1993 Student paper Prize from INCE.

S. Lee and W.C. Meecham, 1993. Quadrupole Directivity of Noise from Homogeneous Turbulence and Turbulent Free Jet as Examples. J. Acoustical Soc. Am. To be published.

S. Lee and W.C. Meecham, 1993. The Numerical Prediction of Noise Generated by a Jet Impinging on a Plate Using Large-Eddy Simulation and the Lighthill Analogy. ASME WAM, NCA-Vol. 15/FED-Vol. 168, p. 101-108, Flow Noise Modeling, Measurement, and Control, New Orleans, December.

R.C. Hall, 1993. Heathrow Tunnels CFD Analysis of Ventilation. WS Atkins Science & Technology, Woodcote Grove, Ashley Road, Epsom, Surrey KT18 5BW, U.K.

A.K. Runchal and S.K. Bhatia, 1993. Flow and Heat Transfer in a Three-Dimensional Cubical Cavity. Second U.S. Congress on Computational Mechanics, August 16-18, Washington, D.C.

A.K. Runchal and S.K. Bhatia, 1993. ASME Benchmark Study: ANSWER Predictions for Backward Facing Step and Lid-Driven Cubical Cavity. CFD Triathlon, ASME FED Summer Conference, June 20-24, Washington, D.C.

S. Lee and W.C. Meecham, 1992. A Computation of Turbulent Flow Field for a Square jet and far Field Aerosound Using Large-Eddy Simulation. Bulletin American Physical Society, 37, 8, Nov. 1992

S. Lee and W.C. Meecham, 1992. A Large-Eddy Simulation of Aerosound Using Homogeneous Turbulence as Example. J. Acoustical Soc of America, 92, 4,Part 2, 124^th Meeting, New Orleans, 31Oct-4 Nov.

Seungbae Lee, 1992. Subgrid-Scale Modeling in Large-Eddy Simulation and its Application to Aerosound. Ph.D. Thesis, Mechanical Engineering, University of California, Los Angeles.

A.K. Runchal, 1992. ANSWER: A Benchmark Study for Backward Facing Step. 1992 WAM, ASME, Anaheim, CA, Nov. 8-13.

M.A. Zook and A.K. Runchal, 1992 Application of Computational Fluid Modeling to the Development of Semiconductor Chemical Vapor Deposition Systems. J. Vacuum Sci. Technology, A 10(4), p. 850-855.

D. Rafinejad, J. Monkowski, L. Wright and A.K. Runchal, 1991. Prediction of Flow and Heat Transfer in a Novel Thermal CVD Reactor. Comp. Techniques and Numerical Heat Transfer on PCs and Workstations, p. 85-92, ASME Book # H00674, Ed. D.W. Pepper, A.P. Emery and M.B. Kelleher.

S. Candel, D. Veynante, F. Lacas, E. Maistret, N. Darabiha and T. Poinsot, 1990. Flamelet Descriptions of Turbulent Combustion. Invited Lecture, 9th International Heat Transfer Conf., Aug. 19-24, 1990, Jerusalem, Israel.

C.E. Janeke, L. Bester and A.K. Runchal, 1990. AIRLINES: A Computational Tool for HVAC Design, To Appear.

P.K.C. Wang, E. Behaegel and A.K. Runchal, 1990. Iterative Solution of a Free-Boundary Problem Arising in Microscopic Particle Manipulation Inside a Liquid Layer. 9th Intn'l Conf. on Analysis and Optimization of Systems, June 12-14, 1990, Antibe, France, Springer Verlag, Berlin.

L.S. Caretto and A. K. Runchal 1989. Ramjet Combustor Mathematical and Engineering Design. Paper # 89-2799, AIAA/ASME/SAE/ASEE 25th Joint Propulsion Conference, July 10, 12, 1989, Monterey, California.

L.S. Caretto and A. K. Runchal 1989. Capabilities of Personal Computers for Numerical Convective Heat Transfer. ASME National Heat Transfer Conference, Aug. 6-9, 1989, Philadel­phia.

M. Cazalens and M. Desaulty, 1989. Implantation dans le Code ECRIN de Technique de Capture de Chocs (FCT). Report # YKC 4685/89, SNECMA, Paris, France.

P. Guevel, O. Hembise, G. Barrot, J.F. Couchouron and T. Godot, 1989. Optimisation des formes d'entree du bassin d'essais des chaluts de Boulogne sur Mer. To appear

G. Karadimas, 1989. Application of Computational Systems to Aircraft Engine Components Development. 9th Intn'l Symp. on Air Breathing Engines, Sept. 3-8, 1989, Athens, Greece.

E. Maistret, N. Darabiha, T. Poinsot, D. Veynante, F. Lacas, S. Candel and E. Esposito, 1989. Recent developments in the coherent Flamelet Descrip­tions of Turbulent Combustion. Numerical Combustion, Springer Verlag, Berlin, pp. 98-117.

R. Shekhar and J.W. Evans, 1989. Mathematical Modeling of Flow in Pachuca (Air-Agitated) Tanks: Masters Thesis, Part II. Dept. of Materials Science and Mineral Engineering, UC Berkeley, CA.

O. Hembise and G. Barrot, 1988. Singularite en T: MVI Technicatome. Report 88.61.73. Principia Recherche Developpeme­nt, S.A., Sophia Antipolis, Nice, France.

O. Hembise and G. Barrot, 1988. Adaptation d'un 3D d'ecoule­ment Turbulent Reactif. SNECMA Contact # 265.898 VY, Phase II Final Report by Principia Recherche Developpement, S.A., Sophia Antipolis, Nice, France.

K.C. Karki, S.V. Patankar, A.K. Runchal, and H. C. Mongia, 1988. Improved Numerical Methods for Turbulent Viscous Recirculating Flows. Aerothermal Modeling Phase II - Final Report. NASA CR-182169, EDR 13519.

S.V. Patankar, A.K. Runchal, and H. C. Mongia, 1988. Improved Numerical Methods for Turbulent Viscous Recirculating Flows. Aerothermal Modeling Phase II - Final Report. NASA CR-182169, EDR 13519.

A.K. Runchal, 1988. ANSWER: A Computational Fluid Dynamics Code from Mainframes to Microcomputers, ASME Computer Applications Symposium, Loyola Marymont University, Los Angeles, October 21.

V.X. Tung, V.K. Dhir, F. Chang, A.R. Karagozian and F. Zhou, 1988 Enhancement of Single Phase Forced Convection Heat Transfer in Tubes and Ducts Using Staged Tangential Flow Injection. Annual Technical Report # 1 (GRI Contract # 5086-260-1535) from UCLA to Gas Research Institute, Chicago, IL.

L.S. Caretto and A. K. Runchal, 1987. Advanced Swirl Concepts Program: Volume II, Literature Survey and Analytical Modeling. Joint project report by ACRi and Marquardt Company, AFWAL-TR-87-2008, U.S. Air Force Wright Aeronautical Lab., May 1987. Restricted Distribution.

A.K. Runchal, 1987. CONDIF: A Modified Central-Difference Scheme for Convective Flows. Int'l J. Num. Methods in Engg., 24. 1593-1608.

A.K. Runchal,, M.S. Anand and H. C. Mongia, 1987. An Uncondi­tionally-Stable Central Differencing Scheme for High Reynolds Number Flows. AIAA-87-0060, AIAA 25th Aerospace Sciences Meeting, Jan. 12-15, 1987, Reno, Nevada.

L.S. Caretto and A. K. Runchal, 1986. Ramjet Combustor Modeling for Engineering Design. JANNAF Propulsion Meeting, New Orleans, August 26-28.

A.K. Runchal, 1986. CONDIF: A Modified Central-Difference Scheme with Unconditional Stability and Very Low Numerical Diffusion. Proc. Eighth Intn'l Heat Transfer Conference, August 17-22, 1986, San Francisco, CA.

N.K. Rizk, A.A. Mostafa and H.C. Mongia, 1986. Modeling of Gas Turbine Fuel Nozzles. ASME Winter Annual Meeting, Dec. 7-12; included in Calculations of Turbulent Reactive Flows, AMD-Vol.81 (1986) Ed. R.M.C. So, J.H. Whitelaw and H.C. Mongia.

B.K. Sultanian and H. C. Mongia, 1986. Fuel Nozzle Air Flow Modeling. AIAA-86-1667, AIAA/ ASME/SAE/ ASEE 22nd Joint Propulsion Conference, June 16-18, 1986, Huntsville, Alabama.

Last Updated: February, 2001

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