High-resolution reynolds-averaged navier-stokes flow predictions over axisymmetric bodies with tapered tails

AIAA Journal

Volumn 47, Issue 1, 2009, Pages 19-32

  Jeans, T L ^a,d   Watt, G D ^b,d   Gerber, A G ^c,d   Holloway, A G L ^c,d   Baker, C R ^c,d  

^a UNITED STATES AIR FORCE ACADEMY   (United States)

^b DEFENCE RESEARCH AND DEVELOPMENT CANADA   (Canada)

^c UNIVERSITY OF NEW BRUNSWICK   (Canada)

^d Department of Aeronautics ^*

Author keywords

[No Author keywords available]

Indexed keywords

AXISYMMETRIC; AXISYMMETRIC BODIES; COMPREHENSIVE STUDIES; COMPUTATIONAL RESULTS; COMPUTATIONAL STUDIES; DIRECT INTEGRATIONS; EXPERIMENTAL UNCERTAINTIES; FORCE DISTRIBUTIONS; HIGH RESOLUTIONS; HYBRID MESHES; HYDRODYNAMIC IMPULSES; LONGITUDINAL FORCES; PARAMETERIZED; REYNOLDS; REYNOLDS STRESSES; SEPARATED FLOWS; STOKES FLOWS; STREAMLINED BODIES; STRESS TRANSPORTS; SURFACE PRESSURES; WALL SHEAR STRESSES;

EXPERIMENTS; FLUID DYNAMICS; FORECASTING; FRICTION; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER; SHEAR STRESS; STRENGTH OF MATERIALS; TURBULENCE MODELS;

BODIES OF REVOLUTION;

EID: 58149377909     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.30911     Document Type: Article

References (39)

1. Munk, M. M., "The Aerodynamic Forces on Airship Hulls," NACA Rept. 184, 1924.
2. Watt, G. D., Tanguay, B., and Cooper, K. R., "Submarine Hydrodynamics in the Wind Tunnel: The DREA Static Test Rig," Warship '91: Royal Institution of Naval Architects International Symposium on Naval Submarines 3, Royal Inst. of Naval Architects, London, May 1991.
3. Watt, G. D., Nguyen, V. D., Cooper, K. R., and Tanguay, B., "Wind Tunnel Investigations of Submarine Hydrodynamics: The Development of the DREA Static Test Rig and Some Results," Canadian Aeronautics and Space Journal, Vol. 39, No. 3, 1993, pp. 119-126.
4. Nguyen, V. D., Drolet, Y., and Watt, G. D., "Interference of Various Support Strut Configurations in Wind Tunnel Tests on a Submarine Model," 33rd Aerospace Sciences Meeting and Exhibit, AIAA Paper 95-0443, Jan. 1995.
5. Van Randwijck, E. F., and Feldman, J. P., "Results of Experiments with a Segmented Model to Investigate the Distribution of the Hydrodynamic Forces and Moments on a Streamlined Body of Revolution at an Angle of Attack or with a Pitching Angular Velocity," Naval Surface Warfare Center Carderock Division, NSWCCD-50-TR-2000/008, Bethesda, MD, Feb. 2000.
6. Pankajakshan, R., Remotigue, M. G., Taylor, L. K., Jiang, M., Briley, W. R., and Whitfield, D. L., "Validation of Control-Surface Induced Submarine Manoeuvring Simulations Using UNCLE," 24th Symposium on Naval Hydrodynamics, Naval Studies Board, Office of Naval Research, Washington, D.C., July 2002, pp. 624-639.
7. Sung, C. H., Rhee, B., and Koh, I. Y., "Validation of Forces, Moments and Stability Derivatives of a Maneuvering Series-58 Bare Hull," 25th Symposium on Naval Hydrodynamics, Vol. 5, Naval Studies Board, Office of Naval Research, Washington, D.C., Aug. 2004, pp. 19-30.
8. Baker, CR., Jeans, T. L., Gerber, A. G., Holloway, A. G. L., and Watt, G. D., "Examination of the Flow Separation Characteristics Around a Streamlined Axisymmetric Shape," 2005 ASME Fluids Engineering Division Summer Meeting and Exhibition, Houston, TX, American Society of Mechanical Engineers Paper FEDSM 2005-77149, June 2005.
9. Forsythe, J. R., Squires, K. D., Wurtzler, K. E., and Spalart, P. R., "Detached Eddy Simulation of Fighter Aircraft at High Alpha," 40th AIAA Aerospace Sciences Meeting and Exhibit, AIAA Paper 2002-0591, Jan. 2002.
10. Morton, S. A., Steenman, M. B., Cummings, R. M., and Forsythe, J. R., "DES Grid Resolution Issues for Vortical Flows on a Delta Wing and an F18C," 41st AIAA Aerospace Sciences Meeting and Exhibit, AIAA Paper 2003-1103, Jan. 2003.
11. Mitchell, A. M., Morton, S. A., Forsythe, J. R., and Cummings, R. M., "Analysis of Delta-Wing Vortical Substructures Using Detached-Eddy Simulation," AIAA Journal, Vol. 44, No. 5, May 2006, pp. 964-972.
12. Nichols, R. H., "Algorithm and Turbulence Model Requirements for Simulating Vortical Flows," 46th AIAA Aerospace Sciences Meeting and Exhibit, AIAA Paper 2008-337, Jan. 2008.
13. Menter, F. R., and Kuntz, M., "Adaptation of Eddy-Viscosity Turbulence Models to Unsteady Separated Flow Behind Vehicles," Aerodynamics of Heavy Vehicles: Trucks, Busses and Trains, edited by R. McCallen, F. Browand, J. Ross, Springer, New York, 2004.
14. Degani, D., "Effect of Geometrical Disturbance on Vortex Asymmetry," AIAA Journal, Vol. 29, No. 4, 1991, pp. 560-566. doi:10.2514/3.59929
15. Schiff, L. B., Degani, D., and Cummings, R. M., "Computation of Three-Dimensional Turbulent Vortical Flows on Bodies at high Incidence," Journal of Aircraft, Vol. 28, No. 11, 1991, pp. 689-699. doi 10.2514/3.46084
16. Degani, D., and Levy, Y., "Asymmetric Turbulent Vortical Flows over Slender Bodies," AIAA Journal, Vol. 30, No. 9,1992, pp. 2267-2273. doi:10.2514/3.11214
17. Allen, H. J., and Perkins, E. W., "Characteristics of Flow over Inclined Bodies of Revolution," NACA RM A50L07,1951.
18. Lamont, P. J., "Pressures Around an Inclined Ogive Cylinder with Laminar, Transitional, or Turbulent Separation," AIAA Journal, Vol. 20, No. 11, 1982, pp. 1492-1499. doi:10.2514/3.51212
19. Ericsson, L. E., and Reding, J. P., "Vortex-Induced Asymmetric Loads in 2D and 3D Flows," 18th AIAA Aerospace Sciences Meeting, Pasadena, CA, AIAA Paper 1980-181 Jan. 1980.
20. Ferziger, J. H., and Peric, M., Computational Methods for Fluid Dynamics, 2nd ed., Springer, Berlin, .1999.
21. Menter, F. R., "Two-equation Eddy Viscosity Turbulence Models For Engineering Application," AIAA Journal, Vol. 32, No. 8, 1994, pp. 1598-1605. doi:10.2514/3.12149
22. Launder, B. E., Reece, G. J., and Rodi, W., "Progress in the Development of a Reynolds-Stress Turbulence Closure," Journal of Fluid Mechanics, Vol. 68, No. 3, Apr. 1975, pp. 537-566.
23. Schneider, G. E., and Raw, M. J., "Control-Volume Finite Element Method for Heat Transfer and Fluid Flow Using Co-Located Variables, Part 1: Computational Procedure," Numerical Heat Transfer, Vol. 11, No. 4, .1.987, pp. 363-390. doi:10.1080/10407788708913560
24. Hutchinson, B. R., Galpin, P. F., and Raithby, G. D., "Application of Additive Correction Multi-Grid to the Coupled Fluid Flow Equations," Numerical Heat Transfer, Vol. 13, No. 2, 1988, pp. 133-147. doi:10.1080/10407788808913608
25. Raw, M. J., "A Coupled Algebraic Multi-Grid method for the 3D Navier-Stokes Equations," Notes on Numerical Fluid Mechanics, Vol. 49, Vieweg-Verlag, Braunschweig, Germany, 1995.
26. Hutchinson, B. R., and Raithby, G. D., "A Multi-Grid Method Based on the Additive Correction Strategy," Numerical Heat Transfer, Vol. 9, 1986, pp. 511-537. doi:10.1080/10407788608913491
27. Raw, M. J., "Robustness of Coupled Algebraic Multi-Grid for the Navier-Stokes Equation," 34th Aerospace and Sciences Meeting and Exhibit, Reno, NV,AIAA Paper 96-0297, Jan. 1996.
28. Baker, C. R., "A Strategic Meshing Approach to Modeling Hydrodynamic Flow Around Streamlined Axisymmetric Shapes," Masters Thesis, Dept. of Mechanical Engineering, Univ. of New Brunswick, New Brunswick, Canada, Mar. 2006.
29. Watt, G. D., Baker, C. R., Gerber, A. G., and Fouts, C., "Scripted Hybrid Mesh Adaptation for High Incidence RANS Flows About Axisymmetric Shapes," 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA Paper 2006-886, Jan. 2006.
30. Watt, G. D., Baker, C. R., and Gerber, A. G., "ANSYS CFX-10.0 RANS Normal Force Predictions for the Series-58 model 4621 Unappended Axisymmetric Submarine Hull in Translation," Defence Research and Development Canada - Atlantic, TM 2006-037, Dartmouth, NS, Canada, Sept. 2006.
31. Simpson, R. L., "Aspects of Turbulent Boundary Layer Separation," Progress in Aerospace Sciences, Vol. 32, Nov. 1996, pp. 457-521. doi:10.1016/0376-0421(95)00012-7.
32. Yates, L. A., and Chapman, G. T., "Streamlines, Vorticity Lines, and Vortices Around Three-Dimensional Bodies," AIAA Journal, Vol. 30, No. 7, 1992, pp. 1819-1826. doi:10.2514/3.11142
33. Wetzel, T. G., and Simpson, R. L., "Measurement of Three-Dimensional Crossflow Separation," AIAA Journal, Vol. 36, No. 4, 1998, pp. 557-564. doi:10.2514/2.429
34. Ahn, S., "An Experimental Study of Flow over a 6 to 1 Prolate Spheroid at Incidence," Ph.D. Dissertation, Aerospace Engineering Dept., Virginia Polytechnic Inst. and State Univ., Blacksburg, VA, 1992.
35. Sarpkaya, T., "Separated Flow About Lifting Bodies and Impulsive Flow About Cylinders," AIAA Journal, Vol. 4, No. 3, 1966, pp. 414-420. doi:10.2514/3.3453
36. Wetzel, T. G., "Unsteady Flow Over a 6 to 1 Prolate Spheroid," Ph.D. Dissertation, Aerospace Engineering Dept., Virginia Polytechnic Inst. and State Univ., Blacksburg, VA, 1996.
37. Jones, R. T., "Properties of Low-Aspect-Ratio Pointed Wings at Speeds Below and Above the Speed of Sound," NACA Report No. 835, 1946.
38. Howe, M. S., Theory of Vortex Sound, Cambridge Univ. Press, New York, 2002.
39. Lamb, H., Hydrodynamics, 6th ed., Dover, New York, 1932.