National Aeronaut Administration (Nasa)

Predicting the Size of Sunspot Cycle 24 on the Basis of Single- and Bi-Variate Geomagnetic Precursor Methods

A Lunar Surface System Supportability Technology Development Roadmap

Review of the Aerodynamic Acceptance Test and Application to Anti-Icing Fluids Testing in the NRC Propulsion and Icing Wind Tunnel

Towards a Formal Semantics of Flight Plans and Trajectories

An Estimate of the Size and Shape of Sunspot Cycle 24 Based on its Early Cycle Behavior using the Hathaway-Wilson-Reichmann Shape-Fitting Function

Anticipating Cycle 24 Minimum and its Consequences

Materials Chemistry Issues in the Development of a Single-Crystal Solar/Thermal Refractive Secondary Concentrator

Method for Measuring Thermal Conductivity of Small Samples Having Very Low Thermal Conductivity

Plasma Sail Concept Fundamentals

Solid Oxide Fuel Cell APU Feasibility Study for a Long Range Commercial Aircraft Using UTC ITAPS Approach. Volume 1; Aircraft Propulsion and Subsystems Integration Evaluation

Aircraft Turbine Engine Control Research at NASA Glenn Research Center

The a(4) Scheme-A High Order Neutrally Stable CESE Solver

Experimental Results From Stitched Composite Multi-Bay Fuselage Panels Tested Under Uni-Axial Compression

DBD Plasma Actuators for Flow Control in Air Vehicles and Jet Engines - Simulation of Flight Conditions in Test Chambers by Density Matching

Effects of Fusion Tack Welds on Self-Reacting Friction Stir Welds

Solar Cycle and Anthropogenic Forcing of Surface-Air Temperature at Armagh Observatory, Northern Ireland

Study and Analyses on the Structural Performance of a Balance

Collocation and Galerkin Time-Stepping Methods

Topology Synthesis of Structures Using Parameter Relaxation and Geometric Refinement

X-Ray Calibration Facility/Advanced Video Guidance Sensor Test

Comparison of Open-Hole Compression Strength and Compression After Impact Strength on Carbon Fiber/Epoxy Laminates for the Ares I Composite Interstage

The Effects of Foam Thermal Protection System on the Damage Tolerance Characteristics of Composite Sandwich Structures for Launch Vehicles

Neural Network Machine Learning and Dimension Reduction for Data Visualization

Static Aeroelastic Effects of Formation Flight for Slender Unswept Wings