ACDL Technical Reports:

• ACDL TR-13-1:
  Peherstorfer, B., Butnaru, D., Willcox, K. and Bungartz, H., "Localized Discrete Empirical Interpolation Method", Aerospace Computational Design Lab, Dept. of Aeronautics & Astronautics, MIT, June 2013.

• ACDL TR-11-1:
  Yano, M. and D.L. Darmofal, "On Dual-Weighted Residual Error Estimates for p-Dependent Discretizations", Aerospace Computational Design Lab, Dept. of Aeronautics & Astronautics, MIT, September, 2011.

• ACDL TR-09-1:
  Yano, M., "Massively parallel solver for the high-order Galerkin least-squares method", MS Thesis, Dept. of Aeronautics & Astronautics, MIT, June, 2009.

• ACDL TR-08-6:
  Israeli, E.R., "Simulations of a passively actuated oscillating airfoil using a Discontinuous Galerkin method", MS Thesis, Dept. of Aeronautics & Astronautics, MIT, August, 2008.

• ACDL TR-08-5:
  Stirling, L.A., "Development of astronautic reorientation methods: A computational and experimental study", PhD Thesis, Dept. of Aeronautics & Astronautics, MIT, June 2008.

• ACDL TR-08-4:
  Mohnot, A., "Solution of fluid-structure interaction problems using a discontinuous Galerkin technique", MS Thesis, CDO, MIT, May, 2008.

• ACDL TR-08-3:
  Wogrin, S., "Model reduction for dynamic sensor steering: A Bayesian approach to inverse problems", MS Thesis, Dept. of Aeronautics & Astronautics, MIT, June, 2008.

• ACDL TR-08-2:
  Barter, G.E., "Shock capturing with PDE-based artificial viscosity for an adaptive, higher-order discontinuous Galerkin finite element method", PhD Thesis, Dept. of Aeronautics & Astronautics, MIT, June 2008.

• ACDL TR-08-1:
  Duffner, J.D., "The effects of manufacturing variability on turbine vane performance", MS Thesis, Dept. of Aeronautics & Astronautics, MIT, June 2008.

• ACDL TR-07-3:
  Bui-Thanh, T., "Model-constrained optimization methods for reduction of parameterized large-scale systems", PhD Thesis, Dept. of Aeronautics & Astronautics, MIT, May 2007.

• ACDL TR-07-2:
  Bui-Thanh, T., Willcox, K. and Ghattas, O., "Model reduction for large-scale systems with high-dimensional parametric input space", Aerospace Computational Design Laboratory, Dept. of Aeronautics & Astronautics, MIT, August 2007. Also, submitted to SIAM J. Sci Comp.

• ACDL TR-07-1:
  Venditti, D.A. and Darmofal, D.L., "Anisotropic grid adaptation for multiple aerodynamic outputs" Aerospace Computational Design Laboratory, Dept. of Aeronautics & Astronautics, MIT, August 2007.

• ACDL TR-06-2:
  Fidkowski, K.J. and Darmofal, D.L., "Output-based adaptive meshing using triangular cut cells" Aerospace Computational Design Laboratory, Dept. of Aeronautics & Astronautics, MIT, October 2006. Also, submitted to Journal of Computational Physics.

• ACDL TR-06-1:
  Oliver, T.A. and Darmofal, D.L., "Analysis of dual consistency for discontinuous Galerkin discretizations of source terms", Aerospace Computational Design Laboratory, Dept. of Aeronautics & Astronautics, MIT, September 2006. Also, submitted to SIAM Journal on Numerical Analysis.

• FDRL TR-03-1:
  Sauer-Budge, A.M., Bonet, J., Huerta, A. and Peraire, J., "Computing bounds for linear functionals of exact weak solutions to Poisson's equation", Aerospace Computational Design Laboratory, Dept. of Aeronautics & Astronautics, MIT, 2003. Also submitted to SIAM Journal on Numerical Analysis.

• FDRL TR-01-1:
  Wong, J.S., Darmofal, D.L. and Peraire, J. "High-order finite element discretization for the compressible Euler and Navier-Stokes equations", FDRL TR-01-1, Dept. of Aeronautics & Astronautics, MIT, April, 2001.

• FDRL TR-99-3:
  Willcox, K. "Reduced-order aerodynamic models for aeroelastic control of turbomachines", Ph.D. Thesis, Dept. of Aeronautics & Astronautics, MIT, November, 1999.

• FDRL TR-99-2:
  Willcox K., Peraire, J. and White, J., 'An arnoldi approach for generation of reduced-order models for turbomachinery', FDRL TR-99-1, submitted to Computers and Fluids, September 1999.

• FDRL TR-99-1:
  Bayt, R., "Analysis, fabrication, and testing of a MEMS-Based micropropulsion system", Ph.D. Thesis, Dept. of Aeronautics & Astronautics, MIT, June, 1999.

• FDRL TR-98-1:
  Elliott, J. "Aerodynamic optimization based on the Euler and Navier-Stokes equations using unstructured grids", Ph.D. Thesis, Dept. of Aeronautics & Astronautics, MIT, May, 1999.

• FDRL TR-97-7:
  Mughal, B. "Integral Methods for Three-Dimensional Boundary Layers", Ph.D. Thesis, Dept. of Aeronautics & Astronautics, MIT, December, 1997.

• FDRL TR-97-6:
  Rathnasingham, R. "System identification and active control of a turbulent boundary layer", Ph.D. Thesis, Dept. of Aeronautics & Astronautics, MIT, May, 1997.

• FDRL TR-97-5:
  Padmanabhan, A. "Silicon micromachined sensors and sensor arrays for shear-stress measurements in aerodynamic flows", Ph.D. Thesis, Dept. of Mech. Eng., MIT, February, 1997.

• FDRL TR-97-4:
  Vailong, H.J.B., "A posteriori bounds for linear functional outputs of hyperbolic partial differential equations", MS Thesis, Dept. of Aeronautics & Astronautics, MIT, February, 1997.

• FDRL TR-97-3:
  Ahn, J., "Analysis and design of axisymmetric transonic flow with linearized three-dimensional flow prediction", Ph.D. Thesis, Dept. of Aeronautics & Astronautics, MIT, February, 1997.

• FDRL TR-97-2:
  Lorkowski, T., "Small-scale forcing of a turbulent boundary layer", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, January, 1997.
  

• FDRL TR-97-1:
  Arkilic, E.B., "Measurement of the mass flow and tangential momentum accommodation coefficient in silicon micromachined channels", Ph.D. Thesis, Dept. of Aeronautics & Astronautics, MIT, December, 1996.

• CASL TR-93-2:
  Modiano, D.L., "Adaptive Mesh Euler Equation Computations of Vortex Breakdown in Delta Wing Flow, Volume II", Ph.D. Thesis, Dept. of Aeronautics & Astronautics, MIT, January, 1993.

• CASL TR-93-1:
  Modiano, D.L., "Adaptive Mesh Euler Equation Computations of Vortex Breakdown in Delta Wing Flow", Ph.D. Thesis, Dept. of Aeronautics & Astronautics, MIT, January, 1993.

• CFDL TR-92-2:
  Vermeersch, S., "Investigation of the F117 Vortical Flow Characteristics Preliminary Results", MS Thesis, Dept. of Aeronautics & Astronautics, MIT, October, 1992.

• CFDL TR-91-5:
  Breuer, K.S., "The Numerical Simulation of Turbulent Channel Flow", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, November, 1991.

• CFDL TR-91-4:
  Sorensen, T.M., "Viscous Airfoil Optimization Using Conformal Mapping Coefficients as Design Variables", MS Thesis, Dept. of Aeronautics & Astronautics, MIT, May, 1991.

• CFDL TR-91-1:
  Drela, M. and Schafer, M., "Experimental and Computational Investigation of Divergent Trailing Edges", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, January, 1991.

• CFDL TR-91-1:
  Poll, P.B., "Full Potential Analysis and Design of Transonic Propellers", MS Thesis, Dept. of Aeronautics & Astronautics, MIT, February, 1991.

• CFDL TR-90-2:
  Landsberg, A., "Adaptation for Vortex Flows using a 3-D Finite Element Solver", MS Thesis, Dept. of Aeronautics & Astronautics, MIT, November, 1990.

• CFDL TR-89-9:
  Lee, K.M., "Numerical Simulation of Hypersonic Flow Over A Blunt Leading Edge Delta Wing", MS Thesis, Dept. of Aeronautics & Astronautics, MIT, October, 1989.

• CFDL TR-89-7:
  Becker, T.M., "Hybrid 3-D Euler/Navier-Stokes Calculations of Transonic Vortex Flows Over the NTF Delta Wing", MS Thesis, Dept. of Aeronautics & Astronautics, MIT, August, 1989.

• CFDL TR-89-5:
  Kallinderis, I., "Adaptation Methods for Viscous Flows", Ph.D. Thesis, Dept. of Aeronautics and Astronautics, MIT, May, 1989.

• CFDL TR-89-4:
  Modiano, D., "Visualization of Three Dimensional CFD Results", MS Thesis, Dept. of Aeronautics and Astronautics, MIT, May, 1989.

• CFDL TR-89-3:
  Giles, M., "Numerical Methods for Unsteady Turbomachinery Flow", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, April, 1989.

• CFDL TR-89-2:
  Loyd, B., "A Semi-Implicit Navier-Stokes Solver and its Application to a Study of Separated Flow about Blunt Delta Wings", Ph.D Thesis, Dept. of Aeronautics & Astronautics, MIT, February, 1989.

• CFDL TR-89-1:
  Perez-Sanches, J.M. and Murman, E.M., "Numerical Simulation of Deceleration of an Axisymmetric Vortex", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, March, 1989.
  

• CFDL TR-88-11:
  Giles, M., "Developments in the Calculation of Unsteady Turbomacinery Flow", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, October, 1988.

• CFDL TR-88-10:
  Murman, E.M., Goodsell, A.M. and Malecki, R.E., "Transsonic Vortical Flow", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, May, 1988.

• CFDL TR-88-9:
  Krouthen, B., "A Numerical Investigation of Hot Streaks in Turbines", MS Thesis, Dept. of Aeronautics & Astronautics, MIT, June, 1988.

• CFDL TR-88-8:
  Lee, K.M. and Murman, E., "A Comparison of Experimental and Preliminary Numerical Results for Close Coupled Canard-Wing", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, May, 1988.

• CFDL TR-88-7:
  Shapiro, R.A., "An Adaptive Finite Element Solution Algorithm for the Euler Equations," Ph.D. Thesis, Dept. of Aeronautics & Astronautics, MIT, May 1988.

• CFDL TR-88-6:
  Lindquist, D.R., "A Comparison of Numerical Schemes on Triangular and Quadrilateral Meshes", MS Thesis, Dept. of Aeronautics & Astronautics, MIT, May, 1988.

• CFDL TR-88-5:
  Pervais, M.M., "Spatio-Temporal Adaptive Algorithm for Reacting Flows", Ph.D. Thesis, Dept. of Aeronautics & Astronautics, MIT, May 1988.

• CFDL TR-88-4:
  Shapiro, R.A., "Prediction of Dispersive Errors in Numerical Solutions of the Euler Equations", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, March, 1988.

• CFDL TR-88-3:
  Murman, E., Modiano, D., Haimes, R. and Giles, M., "Performance of Several CFD Loops on Parallel Processors," Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, March, 1988.

• CFDL TR-88-2:
  Haimes, R., Giles, M., Murman, E. and Modiano, D., "Performance of Implicit Residual Smoothing on Multiprocessor Machines", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, February, 1988.

• CFDL TR-88-1:
  Giles, M., "Non-Reflecting Boundary Conditions for the Euler Equations", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, February, 1988.

• CFDL TR-87-12:
  Miller, R.H., "Research on Rotor Wake Formation in Forward Flight", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, December, 1987.

• CFDL TR-87-11:
  Modiano, D., "Performance of a Common CFD Loop on Two Parallel Architectures", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, November, 1987.

• CFDL TR-87-9:
  Modiano, D., "Performance of a Common CFD Algorithm on the Alliant FX/8", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, September, 1987.

• CFDL TR-87-8:
  Powell, K.G., "Vortical Solutions of the Conical Euler Equations", Ph.D. Thesis, Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, July, 1987.

• CFDL TR-87-6:
  Goodsell, A.M., "3-D Euler Calculations of Vortex Flows Over Delta Wings", MS Thesis, Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, July, 1987.

• CFDL TR-87-5:
  Lee, K.M., "AFWAL Wing Shape Generator", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, June, 1987.

• CFDL TR-87-4:
  Ruffin, S.M., "Solutions for Hypersonic Viscous Flow Over Delta Wings", MS Thesis, Computational Fluid Dynamics Laboratory, Dept of Aeronautics & Astronautics, MIT, May, 1987.

• CFDL TR-87-1:
  Giles, M., "Energy Stability Analysis of Multi-Step Methods on Unstructured Meshes", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, March, 1987.

• CFDL TR-86-6:
  Giles, M., "UNSFLO: A Numerical Method for Unsteady Inviscid Flow in Turbomachinery", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, December, 1986.

• CFDL TR-86-5:
  Roberts, T.W., "Euler Equation Computations for the Flow Over A Hovering Helicopter Rotor", Ph.D. Thesis, Dept. of Aeronautics & Astronautics, MIT, November, 1986.

• CFDL TR-86-4:
  Malecki, R.E., "Euler Equation Calculations for a Cropped Delta Wing Using the Cyber 205", MS Thesis, Dept. of Aeronautics & Astronautics, MIT, August, 1986.

• CFDL TR-86-3:
  Beauchamp, P.P., "Euler Solutions to the Wavy Wall Problem", MS Thesis, Dept. of Aeronautics & Astronautics, MIT, January, 1986.

• CFDL TR-86-2:
  Murman, E.M. and Powell, K.G., "Comparison of Measured and Computed Pitot Pressures in a Leading Edge Vortex From a Delta Wing", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, January, 1986.

• CFDL TR-86-1:
  Loyd, B. and Murman, E.M., "Finite Volume Solution of the Compressible Boundary Layer Equations", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, April, 1986.

• CFDL TR-85-4:
  Allmaras, S.R., "Embedded Mesh Solutions of the 2-D Euler Equations Using A Cell-Centered Finite Volume Scheme", MS Thesis, Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, August, 1985.

• CFDL TR-85-3:
  Bussing, T.R.A., "A Finite Volume Method for the Navier-Stokes Equations with Finite Rate Chemistry", Ph.D. Thesis, Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, August, 1985.

• CFDL TR-85-2:
  Murman, E.M., Rizzi, A. and Powell, K.G., "High Resolution Solutions of the Euler Equations for Vortex Flows", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, May, 1985.
  

• CFDL TR-85-1:
  Murman, E.M. and Abarbanel, S.S., "Impact of Supercomputers on the Next Decade of Computational Fluid Dynamics", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, March 1985.

• CFDL TR-84-5:
  Thompkins, Jr., W.T. and Dirks, P.W., "The Nemesis System Simultaneous Simulation of Computer Architecture, Numerical Algorithms, and Operating Systems", Dept. of Aeronautics & Astronautics, MIT, September, 1984.

• CFDL TR-84-4:
  Murman, E., "Solutions of the Conical Euler Equations for Flat Plate Geometries - Preliminary Results", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, August, 1984.

• CFDL TR-84-2:
  Usab, Jr., W.J., "Embedded Mesh Solutions of the Euler Equation Using A Multiple-Grid Method", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, December, 1983 (Issued May 1984)..

• CFDL TR-84-1:
  Giles, M., "Solution of 1-D Euler Equations Using A Box Method", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, February 1984.

• CFDL TR-83-7:
  Loyd, B., "Calculating C-Grids with Fine and Embedded Mesh Regions", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, December, 1983.

• CFDL TR-83-6:
  Drela, M. and Giles, M., "Conservative Streamatube Solution of Steady-State Euler Equations", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, November, 1983.

• CFDL TR-83-5:
  Roberts, T.W., "Computation of Potential Flows with Embedded Vortex Rings and Applications to Helicopter Rotor Wakes", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, September, 1983.

• CFDL TR-83-4:
  Larson, G.L., "Acceleration of Aerodynamic Design Through Interleaving of Aerodynamic and Optimization Iterations", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, May, 1983.

• CFDL TR-83-3:
  Murman, E. and Bussing, T.R.A., "On the Computation of Boundary Layer and Euler Equation Solutions", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, March, 1983.

• CFDL TR-83-2:
  Murman, E. and Chapman, G., "Aerodynamic Design Using Numerical Optimization", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, February, 1983.

• CFDL TR-83-1:
  Peeters, M.F., "Computational Methods for Aerodynamic Design Using Numerical Optimization", Computational Fluid Dynamics Laboratory, Dept. of Aeronautics & Astronautics, MIT, February 1983.
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  

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