CFD Flow Analysis and Code Validation for the MSFC Eight-Percent ASRM Cold Flow Model Part II
Ascent Aerodynamic Pressure Distributions on WB001
Assessment of Lifting Body Linear Aerospike Plume Effects on Vehicle Aerodynamics
Computational Analysis of Volutes
Reusable Launch Vehicle (RLV) Propulsion Technology
Overview of CFD Analyses Supporting the Reusable Solid Rocket Motor (RSRM) Program at MSFC
Application of Optimization Techniques to Design of Unconventional Rocket Nozzle Configurations
RSRM Chamber Pressure Oscillations: Transit Time Models and Unsteady CFD
3D Object to 2D Image Invariance Technology for Visualization Problems
Weighting for application? A case for composites technology
Adaptive multi-modal control of a low bandwidth active suspension system
The doubling of oil drain intervals on a Daewoo D2366T Engine