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title: Vertical lift aircraft design conference
Aeroelastic Tailoring of a Civil Tiltrotor Configuration
Government Facilities Supporting the ASTOVL/CTOL Common Affordable Lightweight Fighter Project
The MDA/BAe/GEAE/RR ASTOVL/CTOL Technology Demonstrator Team
The Autonomous Scout Rotorcraft Testbed (ASRT), A US Army IPPD Pilot Project
MODUS A High Speed VTOL System Configuration
Conceptual Design and Performance Analysis for a Large Civil Compound Helicopter
ARPA X-32 STOVL/CTOL Affordable Lightweight Fighter Program
Flight Testing the Eagle Eye Tiltrotor Unmanned Air Vehicle
Supplement to Conference Proceedings No. 22 Pre-Print
Trajectory computation Infrastructure based on BADA Aircraft Performance Model
Aerobots as a Ubiquitous Part of Society
Aerobots as a Ubiquitous Part of Society
Proprotor Load Evaluation in Collision Avoidance Maneuver of Tilt Rotor Unmanned Aerial Vehicle
Aerodynamic Characteristics of Two Rotary Wing UAV Designs
Aerodynamic Characteristics of Two Rotary Wing UAV Designs
Ghost Rider, a Slowed-Rotor/Compound Pilot Optional VLA (presentation only)
Risk Reduction Flight Test of a Pre-Production Active Vibration Control System for the MH-60S
Efficient Coupled Fluid-Structure Interaction Approach for Analysis of Rotors in Forward Flight
Preliminary Sizing of 120-Passenger Advanced Civil Rotorcraft Concepts
Preliminary Sizing of120 Passenger Advanced Civil Rotorcraft Concepts
BVI Airloads Prediction Using CFD/CSD Loose Coupling