1–10 von 24 Ergebnissen
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    Generic Lambda Wing Configuration in Compressible Flow: Effect of Highly Integrated Intakes

    Rein, Martin / Gardner, Anthony D. | AIAA | 2015

      Generic Lambda Wing Configuration in Compressible Flow: Effect of Highly Integrated Intakes

      Rein, Martin | Online Contents | 2015
      Beteiligte: Gardner, Anthony D

    HyShot scramjet testing in the HEG

    Gardner, Anthony D. | TIBKAT | 2007

    Dynamic Stall Simulations on a Pitching Finite Wing

    Kaufmann, Kurt / Merz, Christoph / Gardner, Anthony D. | AIAA | 2016

    Investigations of dynamic stall and dynamic stall control on helicopter airfoils

    Gardner, Anthony D. / Technische Universität Clausthal | TIBKAT | 2016

    Boundary-layer transition measurements on Mach-scaled helicopter rotor blades in climb

    Weiss, Armin / Gardner, Anthony D. / Klein, Christian et al. | Springer Verlag | 2017

      Boundary-layer transition measurements on Mach-scaled helicopter rotor blades in climb

      Weiss, Armin / Gardner, Anthony D. / Klein, Christian et al. | Online Contents | 2017

    Dynamic Stall Simulations on a Pitching Finite Wing (AIAA 2016-4166)

    Kaufmann, Kurt / Merz, Christoph / Gardner, Anthony D. | British Library Conference Proceedings | 2016

    Analysis of Dynamic Stall using Dynamic Mode Decomposition Technique

    Mariappan, Sathesh / Gardner, Anthony / Richter, Kai et al. | AIAA | 2013

    Detection of Unsteady Boundary Layer Transition Using Three Experimental Methods

    Richter, Kai / Wolf, C. C. / Gardner, Anthony et al. | AIAA | 2016