Deman Tang

Publications

Papers Published

  1. Tang, Deman and Attar, Peter and Li, Aiqin and Dowell, Earl H., Complex dynamics of a pyranose ring structure molecule attached to an atomic force microscope, Nonlinear Dynamics, vol 45 no. 3-4 (2006), pp. 283 - 303 [s11071-006-0508-9] [abs].
  2. Tang, Deman and Dowell, Earl H., Flutter and limit-cycle oscillations for a wing-store model with freeplay, Journal of Aircraft, vol 43 no. 2 (2006), pp. 487 - 503 [abs].
  3. Tang, Deman and Dowell, Earl H., Aerodynamic flow control of an airfoil with small trailing-edge strips, Journal of Aircraft, vol 43 no. 6 (2006), pp. 1854 - 1866 [1.18969] [abs].
  4. Tang, Deman and Dowell, Earl H., Experimental and theoretical study of gust response for a wing-store model with freeplay, Journal of Sound and Vibration, vol 295 no. 3-5 (2006), pp. 659 - 684 [024] [abs].
  5. Tang, Deman and Attar, Peter and Dowell, Earl H., Flutter/limit cycle oscillation analysis and experiment for wing-store model, AIAA Journal, vol 44 no. 7 (2006), pp. 1662 - 1675 [abs].
  6. Attar, Peter J. and Dowell, Earl H. and Tang, Deman, Modeling the LCO of a delta wing with an external store using a high fidelity structural model, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, vol 2 (2005), pp. 1394 - 1411 [abs].
  7. Tang, Deman and Dowell, Earl H., Reduced order model analysis for two-dimensipnal molecular dynamic chain structure attached to an atomic force microscope, Journal of Dynamic Systems, Measurement and Control, Transactions of the ASME, vol 126 no. 3 (2004), pp. 531 - 546 [1.1789969] [abs].
  8. Tang, Deman and Gavin, Henri P. and Dowell, Earl H., Study of airfoil gust response alleviation using an electro-magnetic dry friction damper. Part 2: Experiment, Journal of Sound and Vibration, vol 269 no. 3-5 (2004), pp. 875 - 897 [S0022-460X(03)00181-0] [abs].
  9. Tang, Deman and Dowell, Earl H., Dynamic analysis of a protein-ligand molecular chain attached to an atomic force microscope, Journal of Vibration and Acoustics, Transactions of the ASME, vol 126 no. 4 (2004), pp. 496 - 513 [1.1804999] [abs].
  10. Tang, Deman and Gavin, Henri P. and Dowell, Earl H., Study of airfoil gust response alleviation using an electro-magnetic dry friction damper. Part 1: Theory, Journal of Sound and Vibration, vol 269 no. 3-5 (2004), pp. 853 - 874 [S0022-460X(03)00180-9] [abs].
  11. Tang, D.M. and Dowell, E.H., Effects of geometric structural nonlinearity on flutter and limit cycle oscillations of high-aspect-ratio wings, Journal of Fluids and Structures, vol 18 no. SUPPL (2004), pp. 291 - 306 [007] [abs].
  12. Tang, D.M. and Yamamoto, H. and Dowell, E.H., Flutter and limit cycle oscillations of two-dimensional panels in three-dimensional axial flow, Journal of Fluids and Structures, vol 17 no. 2 (2003), pp. 225 - 242 [S0889-9746(02)00121-4] [abs].
  13. Attar, Peter J. and Dowell, Earl H. and Tang, Deman, Modeling aerodynamic nonlinearities for two aeroelastic configurations: Delta wing and flapping flag, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, vol 1 (2003), pp. 12 - 22 [abs].
  14. Attar, P.J. and Dowell, E.H. and Tang, D.M., A theoretical and experimental investigation of the effects of a steady angle of attack on the nonlinear flutter of a delta wing plate model, Journal of Fluids and Structures, vol 17 no. 2 (2003), pp. 243 - 259 [S0889-9746(02)00123-8] [abs].
  15. Tang, Deman and Dowell, Earl H., Reduced Order Model Analysis For Two Dimensional Molecular Dynamic Chain Structure Attached To An Atomic Force Microscope, American Society of Mechanical Engineers, Design Engineering Division (Publication) DE, vol 116 no. 2 (2003), pp. 905 - 924 [abs].
  16. Tang, Deman and Gavin, Henri P. and Dowell, Earl H., Theoretical/experimental study of gust alleviation using an electro-magnetic dry friction damper, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, vol 2 (2003), pp. 1092 - 1108 [abs].
  17. Tang, Deman and Li, Aiqin and Dowell, Earl H., Experimental and theoretical study on rolling effectiveness of multiple control surfaces, AIAA Journal, vol 41 no. 2 (2003), pp. 160 - 167 [abs].
  18. Tang, Deman and Dowell, Earl H., Limit-cycle hysteresis response for a high-aspect-ratio wing model, Journal of Aircraft, vol 39 no. 5 (2002), pp. 885 - 888 [abs].
  19. Tang, Deman and Dowell, Earl H., Limit cycle oscillations of two-dimensional panels in low subsonic flow, International Journal of Non-Linear Mechanics, vol 37 no. 7 (2002), pp. 1199 - 1209 [S0020-7462(01)00140-8] [abs].
  20. Tang, Deman and Li, Aiqin and Dowell, Earl H., Transient response study on rolling effectiveness of multiple control surfaces, American Society of Mechanical Engineers, Applied Mechanics Division, AMD, vol 253 no. 1 (2002), pp. 89 - 100 [abs].
  21. Dowell, Earl H. and Tang, Deman, Nonlinear aeroelasticity and unsteady aerodynamics, AIAA Journal, vol 40 no. 9 (2002), pp. 1697 - 1707 [abs].
  22. Tang, Deman and Dowell, Earl H., Experimental and theoretical study of gust response for high-aspect-ratio wing, AIAA Journal, vol 40 no. 3 (2002), pp. 419 - 429 [abs].
  23. Tang, Deman and Kholodar, Denis and Dowell, Earl H., Nonlinear aeroelastic response of a typical airfoil section with control surface freeplay, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, vol 1 no. III (2000), pp. 1514 - 1523 [abs].
  24. Tang, Deman and Dowell, Earl H., Effects of steady angle of attack on nonlinear flutter of a delta wing plate model, American Society of Mechanical Engineers, Applied Mechanics Division, AMD, vol 238 (2000), pp. 37 - 42 [abs].
  25. Tang, Deman and Henry, James K. and Dowell, Earl H., Nonlinear aeroelastic response of delta wing to periodic gust, Journal of Aircraft, vol 37 no. 1 (2000), pp. 155 - 164 [abs].
  26. Tang, Deman and Kholodar, Denis and Dowell, Earl H., Nonlinear response of airfoil section with control surface freeplay to gust loads, AIAA Journal, vol 38 no. 9 (2000), pp. 1543 - 1557 [abs].
  27. Tang, Deman and Dowell, Earl H. and Hall, Kenneth C., Limit cycle oscillations of a cantilevered wing in low subsonic flow, AIAA Journal, vol 37 no. 3 (1999), pp. 364 - 371 [abs].
  28. Tang, Deman and Henry, James K. and Dowell, Earl H., Limit cycle oscillations of delta wing models in low subsonic flow, AIAA Journal, vol 37 no. 11 (1999), pp. 1355 - 1362 [abs].
  29. Tang, Deman and Dowell, Earl H. and Peters, David A., Reduced order aerodynamic models based upon inflow eigenmodes, Journal of the American Helicopter Society, vol 43 no. 4 (1998), pp. 342 - 351 [abs].
  30. Tang, Deman and Dowell, Earl H., Unsteady aerodynamic forces and aeroelastic response for external store of an aircraft, Journal of Aircraft, vol 35 no. 5 (1998), pp. 678 - 687 [abs].
  31. Conner, M. D. and Tang, D. M. and Dowell, E. H. and Virgin, L. N., Nonlinear Behavior of a Typical Airfoil Section with Control Surface Freeplay: A Numerical and Experimental Study, Journal of Fluids and Structures, vol 11 no. 1 (1997), pp. 89 - [0068].
  32. Tang, Deman and Dowell, Earl H., Nonlinear rotor aeroelastic analysis with stall and advanced wake dynamics, Journal of Aircraft, vol 34 no. 5 (1997), pp. 679 - 687 [abs].
  33. Conner, M.D. and Tang, D.M. and Dowell, E.H. and Virgin, L.N., Nonlinear behavior of a typical airfoil section with control surface freeplay: A numerical and experimental study, Journal of Fluids and Structures, vol 11 no. 1 (1997), pp. 89 - 109 [0068] [abs].
  34. Tang, D.M. and Dowell, E.H., Comments on the ONERA stall aerodynamic model and its impact on aeroelastic stability, Journal of Fluids and Structures, vol 10 no. 4 (1996), pp. 353 - 366 [0023] [abs].
  35. Tang, D.M. and Dowell, E.H., Nonlinear response of a non-rotating rotor blade to a periodic gust, Journal of Fluids and Structures, vol 10 no. 7 (1996), pp. 721 - 742 [0050] [abs].
  36. Cizmas, Paul G.A. and Tang, Deman and Dowell, Earl H., Flow about a slotted cylinder-airfoil combination in a wind tunnel, Journal of Aircraft, vol 33 no. 4 (1996), pp. 716 - 721 [abs].
  37. Tang, D.M. and Cizmas, Paul G.A. and Dowell, E.H., Experiments and analysis for a gust generator in a wind tunnel, Journal of Aircraft, vol 33 no. 1 (1996), pp. 139 - 148 [abs].
  38. Tang, Deman and Dowell, Earl H., Damping prediction for hingeless rotor aeroelastic stability with experimental correlation, Journal of Aircraft, vol 33 no. 6 (1996), pp. 1071 - 1078 [abs].
  39. Tang, D. M. and Dowell, E. H., Nonlinear Response of a Non-Rotating Rotor Blade to a Periodic Gust, Journal of Fluids and Structures, vol 10 no. 7 (1996), pp. 721 - [0050].
  40. Tang, D.M. and Dowell, E.H., Response of a nonrotating rotor blade to lateral turbulence part I: theory, Journal of Aircraft, vol 32 no. 1 (1995), pp. 145 - 153 [abs].
  41. Tang, D.M. and Dowell, E.H., Response of a nonrotating rotor blade to lateral turbulence part II: experiment, Journal of Aircraft, vol 32 no. 1 (1995), pp. 154 - 160 [abs].
  42. Tang, D.M. and Dowell, E.H., Damping prediction for a stalled rotor in flap-lag with experimental correlation, Journal of the American Helicopter Society, vol 40 no. 4 (1995), pp. 79 - 89 [abs].
  43. Tang, D.M. and Dowell, E.H., Experimental investigation of three-dimensional dynamic stall model oscillating in pitch, Journal of Aircraft, vol 32 no. 5 (1995), pp. 1062 - 1071 [abs].
  44. Tang, D.M. and Dowell, E.H., Damping prediction for stalled rotor flap-lag stability with experimental correlation, Applied Mechanics Reviews, vol 48 no. 11/2 (1995), pp. 189 -.
  45. Reynolds, Robert R. and Dowell, Earl H. and Tang, Deman and Virgin, Lawrence N., Nonlinear behavior of low aspect ratio panels in subsonic flow: a preliminary study, American Society of Mechanical Engineers, Aerospace Division (Publication) AD, vol 33 (1993), pp. 9 - 12 [abs].
  46. Tang, D.M. and Dowell, E.H., Experimental and theoretical study for nonlinear aeroelastic behavior of a flexible rotor blade, AIAA Journal, vol 31 no. 6 (1993), pp. 1133 - 1142 [abs].
  47. Tang, D.M. and Dowell, E.H., Flutter and stall response of a helicopter blade with structural nonlinearity, Journal of Aircraft, vol 29 no. 5 (1992), pp. 953 - 960 [abs].
  48. Tang, D.M. and Dowell, E.H., Comparison of theory and experiment for nonlinear flutter and stall response of a helicopter blade, Annual Forum Proceedings - American Helicopter Society (1991), pp. 1413 - 1425 [abs].
  49. Tang, D.M. and Dowell, E.H., On the threshold force for chaotic motions for a forced buckled beam, American Society of Mechanical Engineers (Paper) (1988), pp. 7 - 7 [abs].
  50. Tang, D. M. and Dowell, Earl H., EFFECTS OF NONLINEAR DAMPING IN LANDING GEAR ON HELICOPTER LIMIT CYCLE RESPONSE IN GROUND RESONANCE., Journal of the American Helicopter Society, vol 32 no. 1 (1987), pp. 45 - 53 [abs].
  51. Tang, D. M. and Dowell, E. H. and Albright, J. E., DAMPING IN BEAMS WITH MULTIPLE DRY FRICTION SUPPORTS., Journal of Aircraft, vol 24 no. 11 (1987), pp. 820 - 832 [abs].
  52. Tang, D. M. and Dowell, E. H., RANDOM RESPONSE OF BEAMS AND PLATES WITH SLIPPING AT SUPPORT BOUNDARIES., AIAA Journal, vol 24 no. 8 (1986), pp. 1354 - 1361 [abs].
  53. Tang, D. M. and Dowell, E. H., INFLUENCE OF NONLINEAR BLADE DAMPING ON HELICOPTER GROUND RESONANCE INSTABILITY., Journal of Aircraft, vol 23 no. 2 (1986), pp. 104 - 110 [abs].
  54. Tang, D.M. and Dowell, E.H., Damping in beams and plates due to slipping at the support boundaries. II. Numerical and experimental study, J. Sound Vib. (UK), vol 108 no. 3 (1986), pp. 509 - 22 [abs].
  55. Tang, D. M. and Wang, M. Q., COUPLING TECHNIQUE OF ROTOR-FUSELAGE DYNAMIC ANALYSIS., American Society of Mechanical Engineers (Paper) (1983), pp. 4 -.
  56. Tang, D.M. and Ilgamov, M.A. and Dowell, E.H., Buckling and post-buckling behavior of a pipe subjected to internal pressure, Trans. ASME, J. Appl. Mech. (USA), vol 62 no. 3 (0), pp. 595 - 600 [abs].