1–20 von 52 Ergebnissen
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    A Third Approximation to Glauert's Momentum Theory

    Peters, David A | Online Contents | 2016

    Minimum Induced Power for a Rotor with a Finite Number of Blades

    Hong, JunSoo / Peters, David A. | AIAA | 2017

    A State-Space Airloads Theory for Flexible Airfoils

    Peters, David A. | Online Contents | 2007

    DESIGN OF SERVO-FLAP HELICOPTER ROTOR BLADES WITH FORWARD SWEPT WINGTIPS

    Wei, Fu-Shang / Peters, David A. | British Library Conference Proceedings | 2019

    XGBoost Gradient-Boosted Tree Predictions Using Limited Data for Coaxial Rotor Helicopters

    Seidel, Cory A. / Genter, Ethan / Peters, David A. | AIAA | 2021

    Dynamic Stall with Circulation Pulse and Hysteresis for NACA 0012 and VR-12 Airfoils

    Modarres, Ramin / Peters, David A. / Gaskill, Jacob | British Library Conference Proceedings | 2015

    Unified airloads model for morphing airfoils in dynamic stall

    Ahaus, Loren A. / Peters, David A. | Tema Archiv | 2010

    Effects of Cyclic Pitch on Time Delayed Dynamics in Coaxial Rotor Systems

    Genter, Ethan S. / Seidel, Cory A. / Peters, David A. | AIAA | 2021

    Evaluation of Intermediate Values for Coaxial Rotor Helicopter Data Using Gradient Boosted Trees

    Seidel, Cory A. / Genter, Ethan S. / Peters, David A. | AIAA | 2021

    Finite state induced flow models. II - Three-dimensional rotor disk

    Peters, David A. / He, Cheng J. | AIAA | 1995

    EVALUATION OF INTERMEDIATE VALUES FOR COAXIAL ROTOR HELICOPTER DATA USING GRADIENT BOOSTED TREES

    Seidel, Cory A. / Genter, Ethan S. / Peters, David A. | TIBKAT | 2021