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Luftfahrzeug
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Maximum endurance for battery-powered rotary-wing aircraft
Maximum endurance for battery-powered rotary-wing aircraft
Buckling Alleviation for Joined-Wing Aircraft
Buckling Alleviation for Joined-Wing Aircraft
Corrigendum to "Aircraft flight characteristics in icing conditions" [Prog. Aerosp. Sci. 74 62-80]
On the Aerodynamic Efficiency of Insect-Inspired Micro Aircraft Employing Asymmetrical Flapping
Aircraft flight characteristics in icing conditions
Aircraft flight characteristics in icing conditions
Multiphysics simulations in automotive and aerospace applications
Dynamic tests of composite panels of an aircraft wing
Robust Fault-Tolerant Control Allocation for an Input-Redundant Aircraft
Luftfahrzeuge (Luftverkehr): Deutschland, Jahre,Luftfahrzeugart
Trends in development accelerated testing for automotive and aerospace engineering
Sliding Mode Reconfigurable Fault Tolerant Control for Nonlinear Aircraft Systems
Robust Adaptive Fault-Tolerant Control for Hypersonic Flight Vehicles with Multiple Faults
Modeling and Theoretical Design of Missile Launch System Utilizing Electromagnetism
On the Use of Resilience Models as Digital Twins for Operational Support and In-Time Decision Making
Aviation-BERT: A Preliminary Aviation-Specific Natural Language Model
Future Space Propulsion Technologies with Prospects in Africa
Robust Control and Flight Test of a Coaxial Helicopter UAV
Free-Size Optimization of a Stiffened Panel Using Equivalent Radiated Power
Design and Test of an Autonomous Drone SWARM for Chemical Agent Detection
A Consistent Fixed-Point Discrete Adjoint Method for Segregated Navier - Stokes Solvers
An Adaptive Sampling Method for Gradient-Enhanced Surrogate Modeling
Application of Set-Based Design Principles on Multi-Level Aircraft Design Space Exploration
Ethical Human Centered Design: Practical Approaches for Aerospace Engineering Education
AMPHIBIOUS BIOINSPIRED ROBOTS FOR OCEAN OBJECTS IDENTIFICATION
New Conceptual Design of Connecting Metallic Flanges for Space Composite Grid Structures
Development of a Flight Test Data Analyzer for Pixhawk Autopilots
Measurement Results of the ACMU System in Various Research UAVs
Energy Absorbing Additive Structures for Crashworthy Aircraft Seats
Design and Numerical-Experimental Validation of Supports’ Equipment for VEGA-C Launcher
Fusion Insights from Ultrasonic and Thermographic Inspections for Impact Damage Analysis
CONCEPTUAL DESIGN OF MARS OCTASTRUT LANDER FOR LARGE SCALE MASS LANDING