A Discrete and Distributed Steady Blowing Application on a High Reynolds Number Semispan Supercritical Wing Configuration [STUB]

Abstract: The FAST-MAC circulation control model was modified to test an array of steady and unsteady…

A Momentum-Based Indicator for Predicting the Peak Opening Load of Supersonic Parachutes

Abstract: In this paper, a new empirical indicator for predicting the peak opening loads of supersonic…

Characterizing Aerodynamic Damping of a Supersonic Missile with CFD

Abstract: Time accurate solutions of the Euler and Navier{Stokes equations are used as an approach to…

Advanced Symbolic Analysis Tools for Fault-Tolerant Integrated Distributed Systems

Abstract: The project aims to develop advanced model-checking algorithms and tools to automate the verification of…

Design of Buckling-Critical Large-Scale Sandwich Composite Cylinder Test Articles

Abstract: It is well known that the buckling response of thin shell structures can be very…

The Imaging X-ray Polarimetry Explorer (IXPE): Technical Overview [STUB]

Abstract: The Imaging X-ray Polarimetry Explorer (IXPE) will expand the information space for study of cosmic…

Remote Recession Measurements of Wire-Seeded PICA Samples in an Arc-Jet Flow [STUB]

Abstract: Various methods for remote recession sensing of PICA have been developed and several seeding methods…

Initial Results of the Software-Driven Navigation for Station Experiment

Abstract: To enable the next generation of robotic and human exploration of the solar system, improvements…

Simulating the Clamped Tapered Beam Specimen Under Quasi-Static and Fatigue Loading Using Floating Node Method [STUB]

Abstract: As part of the NASA Advanced Composites Project (ACP), a sub-element has been designed to…

Combining Progressive Nodal Release with the Virtual Crack Closure Technique to Model Fatigue Delamination Growth Without Re-Meshing [STUB]

Abstract: The present work summarizes an approach to model mixed-mode 3D fatigue crack growth using the…