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title: Vertical lift aircraft design conference
Current Research Activities in Drive System Technology in Support of The NASA Rotorcraft Program
Cost Analysis for Large Civil Transport Rotorcraft
Research on Structural and Aeroelastic Design of a Hybrid Multi-rotor UAV
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 of120 Passenger Advanced Civil Rotorcraft Concepts
Preliminary Sizing of 120-Passenger Advanced Civil Rotorcraft Concepts
V/STOL Conference, Palo Alto, Calif., June 6-8, 1977, Technical Papers
Supersonic flow computations for an ASTOVL aircraft configuration
Aerodynamic design of the Cal Poly Da Vinci Human-Powered Helicopter
Type 'A' V/STOL - One aircraft for all support missions
STOVL RCS Effects on Propulsion System Design
Model 276 = STOVL Aircraft for Sea-Based Multimission Tactical-Sypport Roles - An Alternative
Converting a C-130 Hercules into a Compound Helicopter: A Conceptual Design Study
Overarching Rotorcraft Commonality Assessment
Rebirth of the Personal Flying Platform
Development of the Mesicopter: A Miniature Autonomous Rotorcraft
Application of Adjoint Optimization Method to Multi-Element Rotorcraft Airfoils
A History of Individual Flying Platforms
A Low-Cost, High-Performance VTOL for the General Aviation Marketplace
Linking a Solid-Modeling Capability with a Conceptual Rotorcraft Sizing Code
Problem Definition for the Joint Transport Rotorcraft
SoloTrek™ XFV™ (Exo-Skeletor Flying Vehicle) -- An Inside Look
Flight testing a V/STOL aircraft to identify a full-envelope aerodynamic model
The Design, Development and Testing of a Turbine Powered Simulator for Hot Gas Ingestion Testing
Influence of Alternative Engine Concepts on LCTR2 Sizing and Mission Profile
Coaxial Compound Helicopter for Confined Urban Operations
Cost Analysis for Large Civil Transport Rotorcraft
AERODYNAMIC CHARACTERISTICS OF TWO ROTARY WING UAV DESIGNS
Methodology for estimating helicopter performance and weights using limited data
The selection of convertible engines with current gas generator technology for high speed rotorcraft
The selection of convertible engines with current gas generator technology for high speed rotorcraft
Experimental investigation of wingtip aerodynamic loading
Overview of the US/UK ASTOVL Program
Comparison of Aero/Propulsion Transition Characteristics for a Joint Strike Fighter Configuration
Numerical and Experimental Second Law Analysis of a Low Thickness High Chamber Wing Profile
Comparison of Hover/Ground-Effect Characteristics for a Joint Strike Fighter Configuration
THE title of this report comes from the Keynote Address to the recent International Powered Lift Conference organised by the Royal
...Attitude and velocity high-gain control of a tilt-trirotor UAV
Configuration E-7 Supersonic STOVL Fighter/Attack Technology Program
Hover Testing of a Large Multi-Element Arc Wing VTOL Research Model
Large lighter-than-air vehicles
Review of the Xb-70 Flight Program