THE PROPOSED WORK WILL ASSIST IN FILLING AN EXISTING RESEARCH GAP IN THE FIELD OF BOUNDARY-LAYER BLEED IN HIGH-SPEED INLETS. THE FLOWPATH LEADING UP TO THE INFLOW PLANE OF THE TURBINE IN A TURBINE-BASED COMBINED-CYCLE INLET IS THE SPECIFIC FOCUS OF
$125,676FY2020National Aeronautics and Space AdministrationNASA
Ohio State University, The, Columbus OH