OPERABILITY PROJECTION OF MAJOR AIRCRAFT COMPONENTS DURING EARLY AIRCRAFT DESIGN
STUDY OF THE BENEFITS OF A SEMI-MORPHING WING CONCEPT
Influence of friction material and brake system strain on the brake air chamber total stroke
EXPERIMENTAL VALIDATION OF NUMERICAL PREDICTION OF WING-PROPELLER AERODYNAMIC INTERACTION
POWER LINE COMMUNICATION APPLIED TO FLIGHT TEST INSTRUMENTATION
A HYBRID DIGITAL-PROPORTIONAL HYDRAULIC ACTUATION SYSTEM FOR AIRCRAFT FLIGHT CONTROL
DESIGN CRITERIA OF A THERMAL MASS FLOW SENSOR FOR AIRCRAFT AIR DATA APPLICATIONS
Experimental Analysis of 14-X B Hypersonic Aerospace Vehicle Compression System (AIAA 2017-2383)
Evaluation of Control Methods for Thermal Roll Forming of Aerospace Composite Materials
SEARCH FOR LESS DISTURBED REGIONS FOR SPACECRAFTS IN PLANETARY SYSTEMS
NAMIDA: Multiparty Conversation Based Driving Agents in Futuristic Vehicle
Orbital Evolution of Planet Around a Binary Star (IAA-AAS-DyCoSS2-14-11-08 — AAS 14-580)
Orbital Evolution of Planet Around a Binary Star (IAA-AAS-DyCoSS2-14-11-08 - AAS 14-580)
Improved Aluminum Passivation for Heavy-Duty Coolants
Multi-Axis Serially Redundant, Single Channel, Multi-Path FBW Flight Control System