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