1–11 von 11 Ergebnissen
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    Wave drag reduction by means of aerospikes on transonic wings

    Rein, M. / Rosemann, H. / Schülein, E. | Tema Archiv | 2009

    Experiments in non-reacting compressible shear layers

    DIMOTAKIS, P. / ROSEMANN, H. | AIAA | 1991

    The Cryogenic Ludwieg-Tube of DLR and its new adaptive wall test section

    Rosemann, H / Stanewsky, E / Hefer, G | AIAA | 1995

    Steady Aerodynamics of Miniature Trailing-Edge Devices in Transonic Flows

    Richter, K. / Rosemann, H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011

    NUM. AND EXP. INVESTIGATIONS ON THE APPLICATION OF VORTEX GENERATORS FOR SHOCK WAVE-/BOUNDARY LAYER-INTERACTION CONTROL

    Krenkel, L. / Rosemann, H. / International Council of the Aeronautical Sciences | British Library Conference Proceedings | 2006

    NUMERICAL INVESTIGATION ON THE AERODYNAMIC EFFECT OF MINI-TEDS ON THE AWIATOR AIRCRAFT CONFIGURATION AT CRUISE CONDITIONS

    Richter, K. / Rosemann, H. / International Council of the Aeronautical Sciences | British Library Conference Proceedings | 2006

    ON TRANSITION DETECTION AT HIGH SUBSONIC FREESTREAM MACH NUMBERS USING THERMORESISTIVE SURFACE SENSORS

    Leuckert, J. / Erdmann, R. / Nitsche, W. et al. | British Library Conference Proceedings | 2011

    ADAPTIVE LOAD REDISTRIBUTION USING MINI-TEDS

    Gardner, A. D. / Nitzsche, J. / Neumann, J. et al. | British Library Conference Proceedings | 2006

      Adaptive load redistribution using mini-TEDs

      Gardner, A.D. / Nitzsche, J. / Neumann, J. et al. | Tema Archiv | 2006

    Aspects of Shock Control and Adaptive Wing Technology

    Stanewsky, E. / Rosemann, H. / Confederation of European Aerospace Societies et al. | British Library Conference Proceedings | 2001

    The Effect of Pressure Gradient and a Non-adiabatic Surface on Boundary Layer Transition Investigated by Means of TSP

    Costantini, M. / Hein, S. / Henne, U. et al. | British Library Conference Proceedings | 2013