Previous Project Overview

  1. Tire
  2.  Further Development of Finite Element Methods for Nonlinear Tire Analysis
    NASA Langley NAS1-18137 11/1/90 Ð 12/1/91
  3. Incompressible II
  4.  Adaptive Schemes for Complex Subsonic 3D-Flow Problems in Arbitrary Domains
    NASA/MSFC NAS8-38404 9/13/89Ð9/12/91
  5. Second Order Tensor
  6.  Second Order Tensor Finite Element
    NASA/MSFC NAS3-3723 9/25/86 - 6/30/90
  7. SRB (Solid Rocket Booster)
  8.  Solid Rocket Booster Internal Flow Analysis by Highly-Accurate Adaptive Computational Methods
    NASA/MSFC NAS8-37682 3/15/88 Ð 3/15/91
  9. Langley HP
  10.  H-P Adaptive Methods for Finite Element Analysis of Aerothermal Loads in High-Speed Flows
    NASA Langley NAS1-08746 10/3/88 Ð 10/31/91
  11. AI (Artificial Intelligence)
  12.  Non-Algorithmic Issues in Automated Computational Mechanics
    AFOSR F49620-89-C-0015 3/1/89Ð2/28/91
  13. FSI I
  14.  Adaptive Computational Methods for Fluid Structure Interaction in Internal Flows
    NASA Lewis NAS3-24849 12/10/85-5/10/86
  15. Chemistry I
  16.  Adaptive Computational Methods for Chemically Reactive Radiative Flows Kirtland AFB
    F29601-86-C-0246 8/1/86-1/31/87
  17. Incompressible I
  18.  Adaptive Schemes for Complex Subsonic 3D-Flow Problems in Arbitrary Domains
    NASA/MSFC NAS8-37621 1/4/88-7/4/88
  19. Rotorcraft I
  20.  Advanced Adaptive Computational Methods for Navier-Stokes Simulations in Rotorcraft Aerodynamics
    NASA Ames NAS2-12911 9/27/88-3/27/89
  21. Operator Splitting I
  22.  A New Approach for Solving Navier-Stokes Equations on Unstructured Grids Based on Adaptive Methods and Operator-Splitting
    NASA Ames NAS2-13000 3/2/89-9/2/89
  23. Goodness I
  24.  Pre- and Post-Processing Techniques for Determining 'Goodness' of Computational Meshes
    NASA/MSFC NAS8-38046 1/18/89-7/18/89
  25. FSI II
  26.  Adaptive Computational Methods for Fluid Structure Interaction in Internal Flows (Phase II)
    NASA Lewis NAS3-25196 5/18/87-5/17/89
  27. Chemistry II
  28.  Adaptive Compuational Methods for Chemically Reactive Radiative Flows (Phase II)
    Kirtland AFB F29601-87-C-0066 9/3/87-1/31/90
  29. Goodness II
  30.  Pre- and Post-Processing Techniques for Determining Goodness of Computational Meshes
    NASA MSFC NAS8-38478 9/11/90 Ð 9/11/92
  31. Rotorcraft II
  32.  Advanced Adaptive Computational Methods for Navier-Stokes Simulations in Rotorcraft Aerodynamics
    NASA Ames NAS2-13285 9/27/90 Ð 9/27/92
  33. Operator Splitting II
  34.  A New Approach for Solving Navier-Stokes Equations on Unstructured Grids Based on Adaptive Methods and Operator Splitting
    NASA Ames NAS2-13221 8/30/90 Ð 8/30/92
  35. Hypersonics
  36.  Analysis of Flow, Thermal and Structural Interaction of Hypersonic Structures Subjected to Severe Aerodynamics Heating
    AFOSR F49602-88-C-0001 11/1/87-10/31/90
  37. Aero-Thermal Loads
  38.  Aero-Thermal Loads in High Speed Flow
    Lockheed PO#X5X018260 3/1/88-12/31/88
  39. LoxPost
  40.  SSME LoxPost Flow Analysis/Fluid Structure Interaction
    Lockheed LM9062290F
  41. Friction
  42.  Computational Methods for Nonlinear Dynamics Problems in Solid and Structural Mechanics
    AFOSR, Bolling AFB F49620-86-C-0051
    Vectorizable Algorithms for Adaptive Schemes for Rapid Analysis of SSME Flows
    NASA/MSFC NASH-85080-B
    Adaptive Computational Methods for SSME Internal Flow Analysis
    NASA/MSFC NA8-36647
    Turbine Rotor-Stator Flow Field Analysis
    LC90E8370F
    Adaptive Finite Element Methods for Analysis of Inviscid Compressible Flows
    Lockheed SM80D7030F
  43. PNS
  44.  Highly Accurate Skin Friction Predictions Using Novel Adaptive Techniques
    Wright-Patterson AFB F33657-90-C-2211 8/1/90 Ð 1/31/90
  45. Store
  46. Multi-bodied CFD Methods
    Wright-Patterson AFB F33615-90-C-3001 9/30/90 - 4/30/94
  47. M&M Friction
  48.  New Micro- and Macroscopic Models of Contact and Friction
    AFOSR, Bolling AFB F49620-91-C-0011 11/1/90 Ð 11/1/93
  49. Fatigue
  50.  Crack Propagation Analysis of Fatigue Crack Propagation
    NASA/HSC SBIR Sol 90-1-0401-0122 1/1/91 Ð 6/30/91