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person:(Anderson, W.)

    Use of age-period-cohort models to estimate effects of vehicle age, year of crash and year of vehicle manufacture on driver injury and fatality rates in single vehicle crashes in New South Wales, 2003-2010

    Anderson, R W G | Online Contents | 2015

    Finite Element Solutions for Turbulent Flow over the NACA 0012 Airfoil

    Anderson, W. Kyle / Ahrabi, Behzad R. / Newman, James C. | AIAA | 2016

    Hydrogen evolution in nickel-water heat pipes

    ANDERSON, W. | AIAA | 1973

    Spatial approaches to moons from resonance relative to invariant manifolds

    Anderson, Rodney L. / Lo, Martin W. | Elsevier | 2014

      Spatial approaches to moons from resonance relative to invariant manifolds

      Anderson, Rodney L. | Online Contents | 2014
      Contributors: Lo, Martin W.

    How thick is the border: the relative cost of Canadian domestic and cross-border truck-borne trade, 2004–2009

    Mark Brown, W. / Anderson, William P. | Elsevier | 2014

    Using Technologies for Higher Axleloads and Longer Trains

    Anderson, E. P. / Harris, W. J. | British Library Conference Proceedings

    A General and Extensible Unstructured Mesh Adjoint Method

    Chad Burdyshaw / W. Anderson | AIAA | 2005

    A numerical study on the use of sulfur hexafluoride as a test gas for wind tunnels

    ANDERSON, W. | AIAA | 1990

    Dynamics of Asteroid 2006 RH120: temporary capture phase

    Lo, Martin W. / Anderson, Brian D. | NTRS | 2018

    The Effect of Ignition System Power on Fast Burn Engine Combustion

    Anderson, Richard W. | SAE Technical Papers | 1987

    Aerodynamic design optimization on unstructured grids with a continuous adjoint formulation

    Anderson, W. / Venkatakrishnan, V. | AIAA | 1997

    Membrane flutter paradox - An explanation by singular-perturbation methods.

    ANDERSON, W. J. | AIAA | 1969

    Direct Exploration of the L2 Isolated Invariant Set Using Isolating Neighborhoods

    Lo, Martin W. / Easton, Robert W. / Anderson, Rodney L | NTRS | 2020

    Recent improvements in aerodynamic design optimization on unstructured meshes

    Nielsen, Eric / Anderson, W. | AIAA | 2001

    Enabling Broad Energy Range Computations at Libration Points Using Isolating Neighborhoods (AAS 19-744)

    Anderson, Rodney L. / Easton, Robert W. / Lo, Martin W. | TIBKAT | 2020

    Numerical study on using sulfur hexafluoride as a wind tunnel test gas

    ANDERSON, W. K. | AIAA | 1991

    Dynamics of Asteroid 2006 RH120: Pre-Capture and Escape Phases

    Anderson, Brian D. / Lo, Martin W. | NTRS | 2016

    Aerodynamic design optimization on unstructured meshes using the Navier-Stokes equations

    Nielsen, Eric / Anderson, W. | AIAA | 1998

      Aerodynamic Design Optimization on Unstructured Meshes Using the Navier-Stokes Equations

      Nielsen, E. / Anderson, W. / AIAA et al. | British Library Conference Proceedings | 1998

    Evaluation of Heat Pipes in the Temperature Range of 450 to 700 K

    Anderson, W. G. | British Library Conference Proceedings | 2005

    Predictive Control Design for an Unmanned Aerial Vehicle

    Anderson, P. W. | British Library Conference Proceedings | 2005

    Oscillatory pressures in an idealized boundary layer with application to cylinder flutter.

    ANDERSON, W. J. | AIAA | 1966

    Solutions of High-order Methods for Three-dimensional Compressible Viscous Flows

    Wang, Li / Anderson, W Kyle / Erwin, Jon | AIAA | 2012

    Intermediate altitude rocket exhaust plumes

    ANDERSON, E. W. | AIAA | 1971

    Recent Improvements in Aerodynamic Design Optimization on Unstructured Meshes

    Eric J. Nielsen / W. Kyle Anderson | AIAA | 2002

    Adjoint-Based Shape Optimization for Electromagnetic Problems Using Discontinuous Galerkin Methods

    Wang, Li / Anderson, W. Kyle | AIAA | 2011

    Sensitivity Analysis for the Compressible Navier-Stokes Equations Using a Discontinuous Galerkin Method

    Wang, Li / Anderson, W Kyle | AIAA | 2011

    Mesh Generation Using Unstructured Computational Meshes and Elliptic Partial Differential Equation Smoothing

    Steve Karman / W. Anderson / Mandar Sahasrabudhe | AIAA | 2006

    Maximum Control Surface Freeplay, Design and Flight Testing Approach on the F-22 AIAA Paper 2007-1767 CD-ROM Number 7

    Anderson, W. / Mortara, S. | British Library Conference Proceedings | 2007

    F-22 Aeroelastic Design and Test Validation AIAA Paper 2007-1764 CD-ROM Number 7

    Anderson, W. / Mortara, S. | British Library Conference Proceedings | 2007

    Development of Equipment for Compacting Soil-Cement into Plastic Molds for Design and Quality Control Purposes

    Sullivan, W. Griffin / Howard, Isaac L. / Anderson, Brennan K. | Transportation Research Record | 2019

    Loop Heat Pipe Radiator Trade Study for the 300-550 K Temperature Range

    Anderson, W. G. / Bienert, W. | British Library Conference Proceedings | 2005

    Effect of Diluent on Gelled MMH Ignition and Dual Flame Behavior

    Lastufka, A. / Solomon, Y. / Anderson, W. | AIAA | 2011

    Finite-Element Solutions for Turbulent Flow over the NACA 0012 Airfoil (Invited)

    Anderson, W. Kyle / Reza Ahrabi, Behzad / Newman, James | AIAA | 2015

    Human power production in a caged situation

    ANDERSON, W. | AIAA | 1974

    Further Experimental Study of a Hypergolically-Ignited Liquid-Liquid Rotating Detonation Rocket Engine

    Kubicki, Stephen W. / Anderson, Wesly / Heister, Stephen D. | AIAA | 2020

      FURTHER EXPERIMENTAL STUDY OF A HYPERGOLICALLY-IGNITED LIQUID-LIQUID ROTATING DETONATION ROCKET ENGINE

      Kubicki, Stephen W. / Anderson, Weslv / Heister, Stephen D. | TIBKAT | 2020

    Control systems for large spacecraft requiring precise stabilization

    Anderson, W. W. | NTRS | 1970

    Engineering estimates for supersonic flutter of curved shell segments

    ANDERSON, W. J. | AIAA | 1970

    ATM attitude control system

    Anderson, W. W. | NTRS | 1967

    Added mass of high-altitude balloons

    ANDERSON, W. | AIAA | 1991

    On lateral cable oscillations of cable- connected space stations

    Anderson, W. W. | NTRS | 1969

    Recent experiments in supersonic regime with electrostatic charges

    ANDERSON, W. | AIAA | 1970

    Engineering estimates for supersonic flutter of curved shell segments

    ANDERSON, W. | AIAA | 1968

    An experimental investigation of the shock layer surrounding a sphere in supersonic flow

    ANDERSON, W. | AIAA | 1964

    An MDO approach to Control-Configured-Vehicle design

    Anderson, M. / Mason, W. | AIAA | 1996

      An MDO Approach to Control-Configured-Vehicle Design

      Anderson, M. / Mason, W. / American Institute of Aeronautics and Astronautics et al. | British Library Conference Proceedings | 1996

    Predicting the contribution of running propellers to aircraft stability derivatives

    Phillips, W. / Anderson, E. | AIAA | 2002

    Safety Enhancements Available by Converting MSG-2 Aircraft Maintenance Programs to MSG-3

    Anderson, Richard W. | SAE Technical Papers | 1999

    Flight test certification of primary category aircraft using TP101-41E sportplane design standard

    Anderson, M. W. | AIAA | 1995

    Some numerical and physical aspects of unsteady Navier-Stokes computations over airfoils using dynamic meshes

    RUMSEY, CHRISTOPHER / ANDERSON, W. | AIAA | 1988

    Automated Mesh Optimization for CFD Simulations

    Aravind Balan / Michael A. Park / W. Kyle Anderson | NTRS

    Sensitivity Derivatives for Plasma Discharge Simulations

    Lange, Kyle / Anderson, W. Kyle | AIAA | 2008

      Sensitivity Derivatives for Plasma Discharge Simulations

      Lange, K. / Anderson, W. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2008

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