1–20 of 42 hits
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    Comparison of Tail Rotor Performance with a Slotted, Natural-Laminar-Flow Airfoil

    Axten, C. / Maughmer, M. | British Library Conference Proceedings | 2023

    A Higher-Order Free-Wake Method for a Helicopter Rotor in Forward Flight Using Distributed Vorticity Elements

    Choephel, T. / Maughmer, M. / American Helicopter Society | British Library Conference Proceedings | 2014

    The Evolution of Sailplane Wing Design

    Maughmer, M. / AIAA / ICAS | British Library Conference Proceedings | 2003

    AIAA-2004-5075 A Free-Wake, Lifting-Surface Model Using Distributed Vorticity Elements

    Bramesfeld, G. / Maughmer, M. / Horstmann, K. | British Library Conference Proceedings | 2004

    Development of an Unsteady Aerodynamic Model for Upstream Miniature Trailing-Edge Effectors

    Coder, J. / Maughmer, M. / Vieira, B. et al. | British Library Conference Proceedings | 2011

    Optimally Scheduled Deployments of Miniature Trailing Edge Effectors for Rotorcraft Power Reduction

    Bae, E.S. / Gandhi, F. / Maughmer, M. et al. | British Library Conference Proceedings | 2009

    An Evaluation of Dynamic Stall Onset Prediction Methods for Rotorcraft Airfoil Design

    Vieira, B. / Maughmer, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2013

    Numerical Validation of the Squire-Young Formula for Profile Drag Prediction

    Coder, J. / Maughmer, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2013

    Winglet Design for Wind Turbines Using a Free-Wake Vortex Analysis Method

    Maniaci, D. / Maughmer, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    One-Equation Transition Closure for Eddy-Viscosity Turbulence Models in CFD

    Coder, J. / Maughmer, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    Scaling wake-particle interactions for aerial applications research

    ORMSBEE, A. / BRAGG, M. / MAUGHMER, M. | AIAA | 1980

    A CFD-Compatible Transition Model Using an Amplification Factor Transport Equation

    Coder, J. / Maughmer, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2013

    Trailing edge flow conditions as a factor in airfoil design

    Ormsbee, A. I. / Maughmer, M. D. | NTRS | 1984

    A class of airfoils having finite trailing edge pressure gradients

    Ormsbee, A. I. / Maughmer, M. D. | NTRS | 1985

    Validation of engineering methods for predicting hypersonic vehicle control forces and moments

    MAUGHMER, M. / OZOROSKI, L. / STRAUSSFOGEL, D. et al. | AIAA | 1993

    INVISCID ANALYSIS OF HORIZONTAL-AXIS WIND TURBINES USING DISTRIBUTED VORTICITY ELEMENTS

    Basom, B. / Maughmer, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011

    Airfoil Design and Testing for High-Lift Rotorcraft Applications

    Martin, P. / Rhee, M. / Maughmer, M. et al. | British Library Conference Proceedings | 2008