Drehschwingungssimulation am Antriebsstrang — Variantenbeherrschung im Nutzfahrzeug
Upgrade of DRAMA - ESA's Space Debris Mitigation Analysis Tool Suite
Race Track Development of a Hydraulic Ride Height Control System
Gravisensing in Single-Celled Systems: Characean Rhizoids and Protonemata
First Experiences with Field Test and Perspectives for Utility Companies
Attenuation of Driveline Vibrations through Tuning of Propeller Shaft Liners
A NOVEL FMI AND TLM-BASED DESKTOP SIMULATOR FOR DETAILED STUDIES OF THERMAL PILOT COMFORT
Trajectory Options for Human Mars Missions AIAA Paper 2006-6308
Incorporating Process Knowledge into Object Recognition for Assemblies
The "Goettinger Modell" - A trichlorethylene vaporizer created by Hosemann / Hickel
Albert Niemann and the cocaine research in Goettingen
Ablative Thermal Response Analysis Using the Finite Element Method
Multiobjective Hypersonic Entry Aeroshell Shape Optimization
INVESTIGATION OF BUBBLE TOPOLOGY IN TUBES WITH CONSTANT BEND RADII IN A MICROGRAVITY ENVIRONMENT
Acoustic Noise Assessment of Gasoline Direct Injection Fuel Injectors Using Taguchi Methods
AIAA-2005-2771 Daedalon: A Revolutionary Morphing Spacecraft Design for Planetary Exploration
Structural Verification and Modeling of a Tension Cone Inflatable Aerodynamic Decelerator
Difficulties making reliability predictions for Si, GaAs, and InP [4215-12]
Computational Aeroelasticity in Aeroelastic Wing Design with reduced Structural Models
Computational Aeroelasticity in Aeroelastic Wing Design with reduced Structural Models
Fixed-focus camera objective for small remote sensing satellites [1940-15]
Progress in Automated Ground Control of ESA's Gaia Mission (AIAA 2018-2603)
2003-01-0840 The Progressive Spin Inlet - Homogeneous Flow Distributions Under Stringent Conditions
Force Measurements on a NACA 0012 Wingtip at Mach 0.75
Content-Aware Packet-Level Interleaving Method for Video Transmission over Wireless Networks
Morphological Aspects of Laserfluorescence-Effects in Dental Caries
Oscillation of Supersonic Inflatable Aerodynamic Decelerators at Mars
AIAA 2006-0732 Zero-Gravity Stability Solutions of Droplets in a Bent Circular Cylinder
Preprocessing Raw Binary Images by Means of Contours
AIAA 2006-0780 An Approximate Ablative Thermal Protection System Sizing Tool for Entry System Design
Variable Angle-of-attack Profile Entry Guidance for a Crewed Lifting Body
The Sequence of Events Generator: A Powerful Tool for Mission Operations
Experimental Determination of Material Properties for Inflatable Aeroshell Structures
Experimental Determination of Material Properties for Inflatable Aeroshell Structures
The Clementine Nickel Hydrogen Common Pressure Vessel Battery
AIAA-2002-5800 Low-cost Lightweight Flight Data Recorders for General Aviation Aircraft
AIAA-2004-6568 Flight System Options for a Long-Duration Mars Airplane
Examining TCP Parallelization Related Methods for Various Packet Losses
Development of the Jupiter Propulsion System
Image sequence analysis of water surface waves in a hydraulic wind wave tank [3804-15]