FUN3D, USM3D ANALYSIS OF THE 4TH AIAA PROPULSION AERODYNAMIC WORKSHOP NOZZLE TEST CASE
FLOW FIELD AND POWER BALANCE OF A DISTRIBUTED AFT-FUSELAGE BOUNDARY LAYER INGESTING AIRCRAFT
Surface Pressure Comparison of an Internal Osculating Waverider Inlet Under Noisy and Quiet Flow
Nacelle 3D Aerodynamic Design and Airframe Integration for an Over Wing Configuration
Multiobjective Aerodynamic Design Optimization of the Contour of Annular Aerospike Nozzles
PIV Measurements of Internal Flows Through Nozzles with Curvature and Shape Transition
SMALL ELECTRICALLY POWERED CONTRA-ROTATING TURBO FAN ENGINES FOR HIGH-SPEED AIRCRAFT APPLICATION
Computational Analysis of an Inlet Ground Vortex Test Case Using CFD++
Effect of Farfield Boundary on Simulations of the Inlet in Crossflow