FUN3D Analyses of the 5th AIAA Propulsion Aerodynamics Workshop Inlet Test Case
Some Design Considerations for Two-Dimensional, Mixed-Compression Inlets for Mach 2.5 to 3.5.
Experimental hypersonic inlet investigation with application to dual-mode scramjet.
Development of a Flow Field for Testing a Boundary-Layer-Ingesting Propulsor
Full Transient Features of Heat Transfer and Sensitivities on Deep Water Wells
Numerical Simulations of a Quiet SuperSonic Technology (QueSST) Aircraft Preliminary Design
Numerical Simulation of Low Engine Order Excitation in a Transonic Compressor
STS Forebody Material Selection Method Using Integrated Aerothermodynamic Optimization Approach
Overview of Boeing's shape memory alloy based morphing aerostructure
A simplified sizing and mass model for axial flow turbines