Bibliography for Neal T. Frink

June 2005

 

Formal Refereed Publications

1.      Frink, N.T., Bonhaus, D.L., Vatsa, V.N., Bauer, S.X.S, Tinetti, A.F., "A Boundary Condition for Simulation of Flow Over Porous Surfaces", Journal of Aircraft, Vol. 40, No. 4, July-August 2003, pp. 692-698.

2.      Frink, N.T., Pirzdeh, S.Z., Parikh, P.C., Pandya, M.J., and Bhat, M.K.: "The NASA Tetrahedral Unstructured Software System (TetrUSS)", The Aeronautical Journal, Vol. 104, No. 1040, October 2000, pp. 491-499

3.      Frink, N.T. and Pirzadeh, S.Z.: "Tetrahedral Finite-Volume Solutions to the Navier-Stokes Equations on Complex Configurations" Int. J. Numer. Meth. Fluids 31 pp. 175-187 (1999) (Conference paper).

4.      Frink, N. T., "Tetrahedral Unstructured Navier-Stokes Method for Turbulent Flows", AIAA Journal , Vol. 36, No. 11, November 1998, pp. 1975-1982 .

5.      Parikh, P.; Pirzadeh, S.; and Frink, N. T.: "Unstructured Grid Solutions to a Wing/Pylon/Store Configuration", Journal of Aircraft , Vol. 31, No. 6, Nov-Dec, 1994, pp. 1291-1296.

6.      Frink, N. T.: "Upwind Scheme for Solving the Euler Equations on Unstructured Tetrahedral Meshes", AIAA Journal , Vol. 30, No. 1, January 1992.

7.      Frink, N. T., Chu, J.; Mercer, C. E.; and Klein, J. R.: “Experimental Study of Analytically and Empirically Designed Vortex Flaps on a 65-Degree Swept Fighter Configuration at Transonic Speeds.” NASA TP 2959, February 1990.

8.      Frink, N. T.: "Wind-Tunnel Wall Effects on Delta Wings", Journal of Aircraft , Vol. 26, No. 5, May 1989, pp. 403-404.

9.      Frink, N. T.: "Experimental Study of an Aspect-Ratio-1.355 Wing-Body Configuration Employing an Analytically Designed Vortex Flap at Mach 0.4." NASA TP 2686, March, 1987.

10.  Frink, N. T.: "A Concept for Designing Vortex Flap Geometries." NASA TP-2233, December 1983.

11.  Lamar, J. E., and Frink, N. T.: "Aerodynamic Features of Designed Strake-Wing Configurations", Journal of Aircraft, August 1982, pp.639-646.

12.  Frink, N. T.: "Lifting Surface Theory for Skewed and Swept Subsonic Wings", Journal of Aircraft , vol. 19, July 1982, pp. 519-524.

13.  Lamar, J. E., and Frink, N. T.: "Experimental and Analytical Study of the Longitudinal Aerodynamic Characteristics of Analytically and Empirically Designed Strake-Wing Configurations at Subcritical Speeds." NASA TP 1803, June 1981.

14.  Frink, N. T., and Lamar, J. E.: "An Analysis of Strake Vortex Breakdown Characteristics in Relation to Design Features", Journal of Aircraft , vol. 18, April 1981, pp. 253-258.

15.  Frink, N. T., and Lamar, J. E.: "Water-Tunnel and Analytical Investigation of the Effect of Strake Design Variables on Strake Vortex Breakdown Characteristics." NASA TP 1676, August 1980.

Referenceable Conference Papers/Presentations

 

16. Pandya, M.J., Frink, N.T., and Noack, R.W.: "Progress Toward Overset-Grid Moving Body Capability for USM3D Unstructured Flow Solver", AIAA 2005-5118, June 2005.

17. Pandya, M.J., Frink, N.T., and Abdol-Hamid, K.S.: "Recent Enhancements to USM3D Unstructured Flow Solver for Unsteady Flows", AIAA 2004-5201, August 2004.

18. Pandya, M.J. and Frink, N.T.: “Agglomeration Multigrid for an Unstructured-Grid Flow Solver”, AIAA 2004-0759, January 2004.

19.  Abdol-Hamid, K.S., Frink, N.T., and Deere, K.A.: “Propulsion Simulations Using Advanced Turbulence Models With Unstructured-Grid CFD Tool, TetrUSS”, AIAA 2004-0714, January 2004.

20.  Lee-Rausch, E.M., Frink, N.T., Mavriplis, D.J., Rausch, R.D., Milholen, R.D.: “Transonic Drag Prediction on a DLR-F6 Transport Configuration Using Unstructured Grid Solvers”, AIAA 2004-0554, January 2004.

21.  Frink, N.T., Bauer, S.X.S, Hunter, C.A., "Simulation of Flows With Passive Porosity", ICAS Paper 2002-2.10.2, presented at the 23rd International Congress of Aeronautical Sciences, Toronto, Canada, September 8-13, 2002.

22.  Pirzadeh, S. and Frink, N. T.: "Assessment of the Unstructured Grid Software TetrUSS for Drag Prediction of the DLR-F4 Configuration", AIAA 2002-0839, January 2002.

23.  Frink, N.T., Bonhaus, D.L., Vatsa, V.N., Bauer, S.X.S, Tinetti, A.F., "A Boundary Condition for Simulation of Flow Over Porous Surfaces" , AIAA 2001-2412, June 2001.

24.  Frink, N.T., Pirzdeh, S.Z., Parikh, P.C., Pandya, M.J., and Bhat, M.K.: "The NASA Tetrahedral Unstructured Software System (TetrUSS)", ICAS Paper No. 0241, keynote paper at the 22nd International Congress of Aeronautical Sciences, Harrogate United Kingdom, Aug. 27-Sept. 1, 2000.

25.  Frink, N. T., Allison, D. O., and Parikh, P. C.: "Unstructured Navier-Stokes Analysis of Wind-Tunnel Aeroelastic Effects on TCA Model 2", NASA/CP-1999-209704/VOL1/PT1, December 1999, pp. 621-640.

26.  Wang, Q., Massey, S. J., Abdol-Hamid, K. S., and Frink, N. T., "Solving Navier-Stokes Equations with Advanced Turbulence Models on Three-Dimensional Unstructured Grids" , AIAA 99-1056, January 1999.

27.  Frink, N. T. and Pirzadeh, S.: "Unstructured Navier-Stokes Analysis of Full TCA Configuration", NASA CP-1999-209692, Vol. 1, Part 1, December 1999, pp. 309-327.

28.  Frink, N. T., "Assessment of an Unstructured-Grid Method for Predicting 3-D Turbulent Viscous Flows" , AIAA 96-0292, January 1996.

29.  Frink, N. T., Pirzadeh, S., and Parikh, P., "An Unstructured-Grid Software System for Solving Complex Aerodynamic Problems" , NASA CP-3291, pp. 289-308, May 9-11, 1995.

30.  Frink, N. T., "Recent Progress Toward a Three-Dimensional Unstructured Navier-Stokes Flow Solver" , AIAA 94-0061, January 1994.

31.  Potsdam, M.A., Intemann, G.A., Frink, N.T., Campbell, R.L., Smith, L.A., and Pirzadeh, S.: "Wing/Pylon fillet Design Using Unstructured Mesh Euler Solvers", AIAA Paper 93-3500, August, 1993.

32.  Frink, N.T., Parikh, P., and Pirzadeh, S.,"Status of VGRID/USM3D Aero Analysis System", NASA CP 10119, Proceedings of Workshop Sponsored by NASA on Unstructured Grid Generation Techniques and Software, April 27-28, 1993, pp. 87-105.

33.  Parikh, P.; Pirzadeh, S.; and Frink, N. T.: "Unstructured Grid Solutions to a Wing/Pylon/Store Configuration Using VGRID3D/USM3D". AIAA Paper 92-4572, August 1992.

34.  Hartwich, P. M. and Frink, N. T.: "Estimation of Propulsion Effects on Transonic Flows Over a Hypersonic Configuration", AIAA Paper 92-0523, January 6-9, 1992.

35.  Frink, N. T.; Parikh, P.; and Pirzadeh, S.: "Aerodynamic Analysis of Complex Configurations Using Unstructured Grids", AIAA Paper 91-3292, September 1991.

36.  Frink, N. T., Parikh, P., and Pirzadeh, S., "A Fast Upwind Solver for the Euler Equations on Three-Dimensional Unstructured Meshes", AIAA 91-0102, January 1991.

37.  Lamar, J.E.; Hallissey, J.B.; Frink, N.T.; Smith, R.H.; Johnson, T.D., Jr.; Pao, J.L; and Ghaffari, F.: "Review of Vortex Flow Flight Projects on the F-106B." AIAA Paper No. 87-2346, Aug. 17-19, 1987.

38.  Frink, N. T.: "Computational Study of Wind-Tunnel Wall Effects on Flow Field Around Delta Wings." AIAA Paper No. 87-2420, Aug. 17-19,1987.

39.  Kline, J. R.; Chu, J.; and Frink, N. T.: "Aerodynamic Assessment of Vortex Flaps on Two Fighter Aircraft Configurations at Transonic Speeds." Vortex Flow Aerodynamics Conference, NASA CP-2417, Oct. 8-10, 1985.

40.  Hallissey, J. B.; and Frink, N. T.: "Aerodynamic Testing and Analysis of Vortex-Flap Configurations for the 5-percent Scale F-106B". Vortex Flow Aerodynamics Conference, NASA CP2417, Oct. 8-10, 1985.

41.  Frink, N. T.: "Critical Evaluation of a Vortex Flap Design Concept Using a 74-Degree Delta Wing Configuration". Vortex Flow Aerodynamics Conference, NASA CP-2417, Oct. 8-10, 1985.

42.  Frink, N. T.: "Refinements of a Vortex Flap Design Method With Systematic Applications." Vortex Flow Aerodynamics Conference, NASA CP-2418 , Oct. 8-10, 1985.

43.  Schoonover, W. E., Jr., Frink, N. T., Hallissey, J. B., and Yip, L. P.: "Subsonic/Transonic Development of Vortex Flaps for Fighter Aircraft." NASA CP-2398, Vol. 2, 1985.

44.  Frink, N. T.: "Analytical Study of Vortex Flaps on Highly Swept Delta Wings." ICAS Paper No. 82-6.7.2. Presented at 13th ICAS/AIAA Aircraft Systems and Technology Conference, August 22-27,1982.

45.  Luckring, J. M.; Schoonover, W. E.; and Frink, N. T.: "Recent Advances in Applying Free Vortex Sheet Theory for the Estimation of Vortex Flow Aerodynamics." AIAA Paper No. 82-0095, Jan. 11-14,1982.

46.  Lamar, J. E.; and Frink, N. T.: "Aerodynamic Features of Designed Strake-Wing Configurations", AIAA Paper No. 81-1214, June 23-25, 1981.

47.  Frink, N. T.; and Lamar, J. E.: "An Analysis of Strake Vortex Breakdown Characteristics in Relation to Design Features", AIAA Paper 80-0326, Jan. 14-16,1980.

48.  Frink, N. T.: "Lifting Surface Theory for Skewed and Swept Subsonic Wings", (AIAA 79-0551) Summary version of earlier paper. Presented at AIAA 15th Annual Meeting and Technical Display, Washington D.C. Feb 6-8,1979 in national student paper competition.

Other Publications and Oral Presentations.

49. Frink, N.T., Pandya, M.J., and Noack, R.: "Implementation of Overset Moving Body Capability into USM3D Unstructured Flow Solver", Presentation to the 7th Symposium on Overset Composite Grid and Solution Technology, Huntington Beach, CA, October 5-7, 2004.

50. Frink, N.T., Parikh, P.C.: "TetrUSS Capabilities for Stability and Control Applications",  Presented at NASA Symposium on Computational Methods for Stablility and Control, Hampton, VA, September 23-25, 2003.

51.  Frink, N.T. and Milholen II, W.E.: “Assessment of the Unstructured Grid Software TetrUSS for Drag Prediction of the DLR-F6 Configuration”, Presentation to the 2nd AIAA CFD Drag Prediction Workshop held at the 21st AIAA Applied Aerodynamics Conference Orlando, Florida June21-22, 2003.

52.  Frink, N. T.: "Three-Dimensional Upwind Scheme for Solving the Euler Equations on Unstructured Tetrahedral Grids." Ph.D. dissertation, Virginia Polytechnic and State University, to be defended September 1991.

53.  Parikh, P. and Frink, N. T.: "An Adaptive Remeshing Procedure for Three-Dimensional Unstructured Grids," Presented at 4th International Symposium on Computational Fluid Dynamics, Davis, CA, September 1991.

54.  Frink, N. T.; Parikh, P.;, and Pirzadeh, S: "Recent Advances in Three-Dimensional Unstructured Grid Methodology", Presented to the NASA Computational Fluid Dynamics Conference, NASA Ames Research Center, Moffett Field, California, March 12-14, 1991.

55.  Frink, N. T.: "Upwind Scheme for Solving the Euler Equations on Unstructured Tetrahedral Meshes", Presented at workshop on "Accuracy of Unstructured Grid Techniques", January 1990.

56.  Frink, N. T.: "Subsonic Wind-Tunnel Measurements of a Slender Wing-Body Configuration Employing a Vortex Flap". NASA TM 89101, June, 1987.

57.  Frink, N. T., Huffman, J. K., and Johnson, T. D., Jr.: "Vortex Flap Flow Reattachment Line and Subsonic Longitudinal Aerodynamic Data on 50-deg. to 74-deg. Delta Wings on Common Fuselage" NASA TM 84618, December 1983.

58.  Frink, N. T.: "Water Tunnel and Analytical Investigation of the Effect of Strake Design Variables on Strake Vortex Breakdown Characteristics in the Presence of Wing-Body." M.S. Thesis, N. C. State University, March 1979.

59.  Dejarnette, F. R., and Frink, N. T.: "Investigation of Aerodynamic Characteristics of Subsonic Wings", Final Report. NASA CR 158661, 1979.

60.  Frink, N. T.: "Lifting Surface Theory for Skewed and Swept subsonic Wings", (Grant No. DAAG 29-76-G-0318) Presented at AIAA Southeast Regional Student Paper Competition, April 1978, winning as best graduate paper.  (subsequently presented in National competition and then published in Journal of Aircraft)

61.  Frink, N. T.; Takallu, M. A.; and DeJarnette, F. R.: "Lifting Surface Theory For Skewed and Swept Subsonic Wings" - Final Report. MAE Dept., N. C. State University, Grant No. DAAG-29-76-G-0318, March 1978.