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15th Aerospace Mechanisms Symposium
25-m-Kombinationen sparen massiv Kraftstoff/Kommentar: Gute Gründe für den Großversuch
2015-2016 SEPMAP Program at NASA JSC: Science, Engineering, and Program Management Training
A 77 GHz eight-channel shaped beam planar reflector antenna
Abbildungsgenauigkeit und Prozeßführung beim IHU. Innenhochdruckumformen
A combined combustion and aftertreatment approach to achieve future emissions standards
A consistent method to design and evaluate the performance of Anti-Roll Tanks for ships
A contact finite element algorithm for the multileaf spring of vehicle suspension systems
A control method for hybrid tilting systems using tilting beams and air spring inclination
Active Generation of Lift Force in the “Wing–Ejector” Integral Aerodynamic Configuration
Active Output Selection for an HEV Boost Maneuver
Adaptable, Deployable Entry and Placement Technology (ADEPT)
Addressing EO-1 Spacecraft Pulsed Plasma Thruster EMI Concerns
A dedicated charger for hybrid energy systems with ultracapacitors and lithium-polymer batteries
A demonstration of prototype near-neat-methanol vehicle controlled fleet test
A design of millimeter-wave radar dynamic range with statistical analysis
A design study of marine current turbine-generator combinations
Advanced active control of contact force between pantograph and catenary for high-speed train
Advanced Components for Cryogenic Integration
Advanced composite turboprops. Modeling, structural, and dynamic analysis
Advanced flywheel energy storage unit for a high power energy source for vehicular use
Advances in Aircraft System Identification at NASA Langley Research Center
Advances on railway yaw damper characterisation exposed to small displacements
Advance study of an Application Technology Satellite /ATS-4/ mission Final report
Advance Study of an Application Technology Satellite (Ats-4) Mission Final Report
Aero- and Thermodynamic Analysis of SHEFEX I
Aerodynamic Characteristics of Hypersonic Flight Experiment (HYFLEX) Vehicle
Aerodynamic Compensation Methods for Aeroelastic Divergence of Forward-Swept Wing
Aerodynamic noise reduction using porous materials and their application to high-speed pantograph
Aerothermal prediction of multiple hot jets in crossflow for aircraft applications