Biomimetic Adaptive Airframe Technology (BAAT) for Rotorcraft Design and Optimization
Biomimetic Adaptive Airframe Technology (BAAT) for Rotorcraft Design and Optimization
DEVELOPMENT OF “ARIA”, A COMPACT, ULTRA-QUIET PERSONAL ELECTRIC HELICOPTER
DEVELOPMENT OF ``ARIA'', A COMPACT, ULTRA-QUIET PERSONAL ELECTRIC HELICOPTER
The Development of the Integral Skin Foam Console Arm Rest
Integrated Chassis Control for Improving On-Center Handling Behavior
Modeling and Validation of Lithium-Ion Automotive Battery Packs
Hybrid Electric Propulsion System for Middle Size UAV
Development of Advanced Light-Duty Powertrain and Hybrid Analysis Tool
Closed-loop Active Flow Control of Stall Separation using Synthetic Jets
Planning and Controlling Railway Noise in a Metropolis: Our Practical Experience
2012-3050 Separation Control Characteristics of Synthetic Jets with Circular Exit Array
Ergonomic Design of a Main Control Room of Radioactive Waste Facility Using Digital Human Simulation
Engine Room Lay-out Study for Fuel Efficiency and Thermal Performance
Development and Evaluation of User Interfaces for Situation Observability in Life Support Systems
Electric Field Measurements in Gases Using Cavity Enhanced Polarimetry
NON-SINUSOIDAL TRAJECTORY OPTIMIZATION OF FLAPPING AIRFOIL USING UNSTEADY ADJOINT APPROACH
Shape and Trajectory Optimization of Flapping Airfoil
RE-DESIGN OF BOUNDARY LAYER INGESTING OFFSET INLET VIA PASSIVE FLOW CONTROL MANNER
SUPERSONIC BI-DIRECTIONAL FLYING WING, PART II: CONCEPTUAL DESIGN OF A HIGH SPEED CIVIL TRANSPORT
Heat Flux Measurement Techniques over the Protuberance at the Hypersonic Flow of Mach 7
A Screening Attenuation Evaluation Method for HEV Power Cable
Flow Past a Yawed Rectangular Cavity at Transonic and Low Supersonic Flows
Criteria to Estimate the Effect of Static Stability Margin on Aircraft HQ
Abrupt Response Criteria for Directional Control AIAA Paper
Criterion to Estimate Optimum Lateral Static Stability Margin AIAA Paper
Identify/Utilize Process Capability Information to Predict Variation in Aircraft Early Design
Multiview autostereoscopic display of 36 view using an ultrahigh-resolution LCD [6490A-27]
Advanced Math-Based Engine Calibration and Control System Design
AIAA-2006-5359 The Intelligent VoIP Communication System
2006-01-1022 Vehicle Stability through Integrated Active Steering and Differential Braking
AIAA-2006-2033 Statistical Analysis Tools for Detection of Non-Linearity in Aeroelastic Phenomena
AIAA-2006-1869 Over the Failure, MLGSST for T-50 Supersonic Jet Trainer
AIAA-2006-5355 Automated Communication, Ocean, and Meteorological Satellite Operational Orbit System
AIAA-2006-5356 Analysis of Wheel Off-Loading Strategy of COMS
AIAA-2006-6497 Analysis of Requirements for Directional Dynamics