Cover of Towards Effective Flow Control and Mitigation of Shock Effects in Aeronautical Applications

Legal full-text edition

Towards Effective Flow Control and Mitigation of Shock Effects in Aeronautical Applications

Unknown author · 2025

Transitional Shock Wave Boundary Layer Interaction High-Fidelity CFD Supersonic Boundary-Layer Control Unsteady Separated Flows Reduced-Order Modeling Unsteady Wall-Pressure Measurements Transonic Interaction and Morphing

Read now OAPEN

Rights
Public-domain status shown for GLOBAL. OAPEN open-access record with explicit license: CC-BY