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design
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Länge läuft ... : NGT : die Stadtbahn für Dresden : mehr Platz, mehr Komfort, mehr Fahrkultur
Spanwise Adaptive Wing - PTERA Flight Test
Low-Thrust Transfers from Distant Retrograde Orbits to L2 Halo Orbits in the Earth-Moon System
MDO Problem Suite V3: We have the technology, we can rebuilt it!
PERSEUS - Post-Emergency Response and Surveillance UAV System
Development of an Inertia Relief Method for Aircraft with Dissimilar Engines in LEAPS
VSP-CAD-CFD Interaction and Advanced Modeling Techniques
Analysis of High-Speed Aerodynamics of a Swept Wing with Seamless Flaps
History and Status of the CDISC Aerodynamic Design Method
Multidisciplinary Design Optimization of Low-Boom Supersonic Aircraft with Mission Constraints
Preliminary overall aircraft design with hybrid laminar flow control
Virtual Reality and Virtual Reality Sickness: Creation of a Virtual Reality Sickness Reduction Tool
General Mission Analysis Tool (GMAT)
Design of lower limb and spinal column for TAMUK huamanoid
Design Limit Loads and Verification Approach for the TESS Observatory
About the process of designing railway infrastructure
Design and manufacture of upper limbs for TAMUK humanoid
Overview and Performance of the LOFTID Instrumentation Suite
Topology Optimization of Low-Speed Aeroelastic Wind Tunnel Models
Entry, Descent, and Landing technological barriers and crewed MARS vehicle performance analysis
Trajectory Design to Mitigate Risk on the Transiting Exoplanet Survey Satellite (TESS) Mission
Influence of Dynamic Flap Movement on Maximum Lift and Wake Vortex Evolution
Design and Performance of an Adaptable Aircraft Manufacturing Concept
Techniques for Conducting Effective Concept Design and Design-to-Cost Trade Studies
A Modular Multiphysics Simulation Framework
Privacy Framework for Social Robots in the Context of User-centered Design
Handling Qualities Optimization for Rotorcraft Conceptual Design
Structural Design and Aeromechanical Analysis of Unconventional Blades for Future Mars Rotorcraft
Organizational Design: The Hybrid (Virtual Offsite / Traditional 'Brick and Mortar') Organization
Overview Of Additively Manufactured TPS Proposed Flight Test And Earth Re-entry Capsule Design
Fixed- and Free-Mode Flutter Derivatives during Aeroelastic Optimization
Spacecraft Material Characterization Using Reflectance Spectra Extracted from RGB/IR Color Images
Overview of Ablation Modeling at NASA
Commercial High Speed Market Study(s) Summary
What it Takes to Conceive, Mature and Mission Infuse Entry and TPS Technologies at NASA
Spacecraft Loads and Acoustic Measurement (SLAM) Attached ESPA Payload, A Goddard IRAD
NASA Langley Research Center Flight Simulation Facilities Overview
Status of Learjet Flight Test and Jet Noise Modeling
Ground Testing of the MISSE-16 Materials