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State-of-the-ART Study for High-Speed Deceleration and Stabilization Devices Final Report
Identification and Testing of Measures to Improve Work Zone Speed Limit Compliance
Evaluation of Unmanned Radar Installations
Traffic Operations and Safety Benefits of Active Traffic Strategies on TxDOT Freeways
Speed Harmonization and Peak-Period Shoulder Use to Manage Urban Freeway Congestion
Effectiveness of Stationary Police Vehicles with Blue Lights in Freeway Work Zones, Summary
Examining the Impact of ASE (Automated Speed Enforcement) in Work Zones on Driver Attention
Aerodynamic Characteristics of Gd B-15B Booster During Cruise and Landing M Equals 0.2
Reducing Lane and Shoulder Width to Permit an Additional Lane on a Freeway: Technical Report
Analysis of Low-Speed Stall Aerodynamics of a Swept Wing with Laminar-Flow Glove
Analysis of Low Speed Stall Aerodynamics of a Swept Wing with Laminar Flow Glove
Lift-TO-Drag Ratios of Slender Wings at Hypersonic Speeds
Space Shuttle Aerodynamic Characteristics of the Nr delta Wing Orbiter, M Equals 0.6 to 1.3
Maximum Lift-TO-Drag Ratios of a Slender, Flat-Top, Hypersonic Bodies, Part 1
Dynamic Speed Adaptation Based on Information Technology: A Theoretical Background
Safety and Operational Impacts of Raising the Speed Limit to 65 MPH
Wing Divergence of Trimmed Aircraft
Letter Report of Evaluation of the Curtiss-Wright All-Mechanical Speed Control
Effects of Cavitation and Ventilation on High-Speed Craft Performance
One-Dimensional Approach to the Maximum Lift- TO-Drag Ratio of a Slender, Flat-Top, Hypersonic Wing
Agile Port and High Speed Ship Technologies, Vol 1: FY05 Projects 3-6 and 8-10
Analysis of Trim and Compressibility Effects in Extended Formation Flight
What Do Drivers Say They Use Speedometers and Tachometers For
Statistical Validation of Speeds and Travel Times Provided by a Data Services Vendor
Optical Communications in Support of Science from the Moon, Mars, and Beyond
Statistical Analysis of CFD Solutions From the Fifth AIAA Drag Prediction Workshop
Two-Dimensional Approach to the Maximum Lift- TO-Drag Ratio of a Slender, Flat-Top, Hypersonic Wing
Field Testing of Eco-Speed Control Using V2I Communication
Agile Port and High Speed Ship Technologies. FY 2008 Final Program Plan
The Use of Known Flow Fields as an Approach to the Design of High Speed Aircraft
Microscope-on-Chip Using Micro-Channel and Solid State Image Sensors