World's Best Scientists 2026 revealed!
Mark Drela

Mark Drela

D-Index & Metrics

Mechanical and Aerospace Engineering

D-Index
35
Citations
8395
World Ranking
2605
National Ranking
919

Best Publications

  • XFOIL: An Analysis and Design System for Low Reynolds Number Airfoils

    Unknown

  • Viscous-inviscid analysis of transonic and low Reynolds number airfoils

    Mark Drela;Michael B. Giles

  • Power Balance in Aerodynamic Flows

    Mark Drela

  • Two-Dimensional Transonic Aerodynamic Design Method

    Michael B. Giles;Mark Drela

  • Implicit Large Eddy Simulation of transition to turbulence at low Reynolds numbers using a Discontinuous Galerkin method

    A. Uranga;P.-O. Persson;M. Drela;J. Peraire

  • Development of the D8 Transport Configuration

    Mark Drela

  • Integrated simulation model for preliminary aerodynamic, structural, and control-law design of aircraft

    Unknown

  • Boundary layer ingestion propulsion benefit for transport aircraft

    David K. Hall;Arthur C. Huang;Alejandra Uranga;Alejandra Uranga;Edward M. Greitzer

  • Flight Vehicle Aerodynamics

    Unknown

  • Two-dimensional transonic aerodynamic design and analysis using the Euler equations

    Unknown

  • Airframe Design for "Silent Aircraft"

    James Hileman;Zoltan Spakovszky;Mark Drela;Matthew Sargeant

  • Boundary Layer Ingestion Benefit of the D8 Transport Aircraft

    Alejandra Uranga;Mark Drela;Edward M. Greitzer;David K. Hall

  • Airframe Design for Silent Fuel-Efficient Aircraft

    J. I. Hileman;Z. S. Spakovszky;M. Drela;M. A. Sargeant

  • Newton solution of coupled viscous/inviscid multielement airfoil flows

    Unknown

  • ISES - A two-dimensional viscous aerodynamic design and analysis code

    Mark Drela;Michael Giles

  • Preliminary Experimental Assessment of the Boundary Layer Ingestion Benefit for the D8 Aircraft

    Alejandra Uranga;Mark Drela;Edward M. Greitzer;Neil A. Titchener

  • Low-Reynolds-number airfoil design for the M.I.T. Daedalus prototype- A case study

    Unknown

  • Analysis of the Aerodynamic Benefit from Boundary Layer Ingestion for Transport Aircraft

    Alejandra Uranga;Alejandra Uranga;Mark Drela;David K. Hall;Edward M. Greitzer

  • On The Construction of Aircraft Conceptual Geometry for High-Fidelity Analysis and Design

    Unknown

  • Newton solution of direct and inverse transonic Euler equations

    M. Giles;M. Drela;W. Thompkins

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