FUN3D Analyses of the 5th AIAA Propulsion Aerodynamics Workshop Inlet Test Case
An investigation of splitter plates for supersonic twin inlets
Some Design Considerations for Two-Dimensional, Mixed-Compression Inlets for Mach 2.5 to 3.5.
Some Design Considerations for Two-Dimensional, Mixed-Compression Inlets for Mach 2.5 to 3.5
FUN3D Analyses in Support of the 5th Propulsion Aerodynamics Workshop (PAW5) - Inlet Test Case
IN-FLIGHT GAINS REALIZED BY MODIFYING A TWIN SIDE-INLET INDUCTION SYSTEM
FUN3D Analyses of the 5th AIAA Propulsion Aerodynamics Workshop Inlet Test Case
LTN Inlets and Nozzles Branch Overview; NASA GE - Methods Development Review
Experimental hypersonic inlet investigation with application to dual-mode scramjet.
Effects of Spent Cooling and Swirler Angle on a 9-Point Swirl-Venturi Injector
Development of a Flow Field for Testing a Boundary-Layer-Ingesting Propulsor
Numerical Simulations of a Quiet SuperSonic Technology (QueSST) Aircraft Preliminary Design
Some pressure-drag effects of rounding the leading edges of hypersonic inlets
Aerodynamic principles for the design of jet- engine induction systems