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Standsicherheit
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keywords:(Standsicherheit)
СУМІШЕВІ ПАЛИВА НА ОСНОВІ ВУГЛЕВОДНЕВО-СПИРТОВОЇ КОМПОЗИЦІЇ
Сhoice of materials for producing dimensionally stable load-carrying structures
Новий підхід до визначення осьових критичних навантажень оболонок, пластин і стрижнів
Апробація методики оцінки фізичної стабільності автомобільних бензинів
Zwei neue zerstörungsfreie Meßverfahren. Zur Verkehrssicherheit von Bäumen
Zulaessige Abweichung der Stuetzlage bei einem Fahrzeug mit vier Stuetzen
Zoning and an Account for Soil Salination in the Design of Automobile Roads
Zielschächte U4 Hamburg. Besonderheiten einer Vereisungsmaßnahme
Yaw Stability Control of Tractor Semi-Trailers
Yaw Stability Control and Emergency Roll Control for Vehicle Rollover Mitigation
Yaw/Roll Stability Modeling and Control of HeavyTractor-SemiTrailer
Yaw rate control of an air bearing vehicle
Yaw rate and side-slip control considering vehicle longitudinal dynamics
Yaw damper modelling and its influence on railway dynamic stability
Yaw-control efficiency analysis for a diamond wing configuration with outboard split flaps
Yaw-control efficiency analysis for a diamond wing configuration with outboard split flaps
Yaw-control efficiency analysis for a diamond wing configuration with outboard split flaps
Yaw Center Control of a Vehicle Using Rear Wheel Steering
Yaw Axis Stability Augmentation System Flight Test Report
Yaw Axis Control as a Means of Improving V/STOL Aircraft Performance
Yaw and lateral stability control based on predicted trend of stable state of the vehicle
YAV-8B Simulation and Modeling. Volume 2: Program Listing
YAV-8B Simulation and Modeling. Volume 1: Aircraft Description and Program Summary
Xc-142A V/STOL Transport Tri-Service Limited Category I Evaluation
Xb-70 Aerodynamic, Geometric, Mass, and Symmetric Structural Mode Data
Xb-70 Aerodynamic, Geometric, Mass, and Symmetric Structural Mode Data
X-48B Flight Research - Test Progress and Instrumentation Needs for the Future
X-43A Flight-Test-Determined Aerodynamic Force and Moment Characteristics at Mach 7.0
X-38 Application of Dynamic Inversion Flight Control
X-33 Attitude Control Using the XRS-2200 Linear Aerospike Engine
X-33 Attitude Control System Design for Ascent, Transition, and Entry Flight Regimes
X-33 Ascent Flight Controller Design by Trajectory Linearization: A Singular Perturbational Approach
X-33 Ascent Flight Controller Design by Trajectory Linearization: A Singular Perturbational Approach
X-33 Ascent Flight Controller Design by Trajectory Linearization: A Singular Perturbational Approach
X-31 Quasi-Tailless Flight Demonstration
X-31A Quasi-Tailless Flight Test Results
X-31 Aerodynamic Characteristics Determined from Flight Data
X-29 Flight Control System: Lessons Learned
X-29A Technology Demonstrator Flight Test Program Overview