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Aircraft Certification by Analysis (CbA): 20-year Vision for Virtual Flight Testing
Helicopter Rotor Blade Flutter - CANCELLED
S-92 - Design for Minimum Operating Costs
Shaft Driven Lift Fan for Common Affordable Lightweight Fighter
ARPA X-32 STOVL/CTOL Affordable Lightweight Fighter Program
Northrop Grumman STOVL/CTOL Affordable Lightweight Fighter
Flight Testing the Eagle Eye Tiltrotor Unmanned Air Vehicle
Full Scale Flight Acoustics Results for the UH-60A Airloads Aircraft
The Direct Lift ASTOVL Aircraft
Integrated Product and Process Development (IPPD) for Dual-Use VTOL Aircraft
Development of a Tiltrotor Autopilot System
Rotor Blade Deicing Using Advanced Blade Control
The Revolutionary Vertical Lift Technology (RVLT) Project
Overview of STOVL Aircraft Propulsion Research Offtakes and Vertical Lift Systems
Propulsion Control Design For A STOVL Integrated Flight/Propulsion Control System
Technology Needs for Future US Navy/Marine Corps Heavy Lift VTOL Aircraft
Aerodynamic Characteristics of Two Rotary Wing UAV Designs
Design Methodology and Analysis of Composite Blades for a Low Weight Rotor
Ghost Rider, a Slowed-Rotor/Compound Pilot Optional VLA (presentation only)
Sikorsky Design Concepts for NASA Heavy Lift Rotorcraft Systems Investigation