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Jay Carter, Founder &
Design, Modelling and Control of a Space UAV for Mars Exploration
Adventures in Low Disk Loading VTOL Design
Development of a Helicopter Vortex Ring State Warning System Through a Moving Map Display Computer
WYVER Heavy Lift VTOL Aircraft
US 2005/0151003 A1 Churchman (43) Pub
Introduction of the M-85 High-Speed Rotorcraft Concept Robert H
Cash Flow Analysis in the Engineering Field, Cash Flow Analysis Is Most Commonly Used in Describing the Predicted Profitability of a Project
A Qualitative Introduction to the Vortex-Ring-State, Autorotation, and Optimal Autorotation
'\, ~ National Advisory Committee for Aeronautics
Mars Science Helicopter: Conceptual Design of the Next Generation of Mars Rotorcraft
Designing Evtol for Urban Air Mobility
A Qualitative Introduction to the Vortex-Ring-State, Autorotation, and Optimal Autorotation
Helicopter Controllability. Reference 2 Presents a Comprehensive History and References 1 and 3 Present Summarized Histories of Helicopter Development
Performance and Hub Vibrations of an Articulated Slowed-Rotor Compound Helicopter at High Speeds
Blade Twist Effects on Rotor Behaviour in the Vortex Ring State
Motivations and Preliminary Design for Mid-Air Deployment of a Science Rotorcraft on Mars
Open Choephel Dissertation.Pdf
Top View
Gyro Terms Rev 2
Influence of Individual Interactions on Helicopter Blade-Vortex Interaction Noise
Investigation of Performance, Loads, and Vibrations of a Coaxial Helicopter in High Speed-Flight
Relationship Between Rotor Wake Structures and Performance Characteristics Over a Range of Low-Reynolds Number Conditions THESIS
A Comparison of Multicopter Noise Characteristics with Increasing Number of Rotors
The Attributes of a Variable-Diameter Rotor System Applied to Civil Tiltrotor Aircraft
Teknofest Aerospace and Technology Festival
The Cutting Edge in Tiltrotor Technology Flying Further, Higher, Faster
An Advanced Mars Helicopter Design
Military Helicopters
TVF WG 2 Technical Report
1 Introduction
ROTATING BLADES and AERODYNAMIC SOUND T
Data and Performances of Selected Aircraft and Rotorcraft Antonio Filippone*
Mars Science Helicopter Conceptual Design
Vortex Ring State a USHST Airmanship Safety Bulletin (Part 1)
Helicopter Flying Handbook (FAA-H-8083-21B) Glossary & Index
Study and Optimization of a Contra-Rotating Propeller Hub for Convertiplanes Part 1: Vto and Hovering
Aerodynamic Performance of an Octorotor SUAV with Different Rotor Spacing in Hover
Airmanship Bulletin the Vuichard Recovery
NASA Heavy Lift Rotorcraft Systems Investigation
Development of a Non-Flapping Rotor System Utilizing Inflexible Blades and Employing a New Rotor Control Mechanism
ABSTRACT PERFORMANCE and LOADS of VARIABLE TIP SPEED ROTORCRAFT at HIGH ADVANCE RATIOS Graham M. Bowen-Davies Doctor of Philosop
PHASE I FINAL REPORT NIAC/USR Grant No. 07600-028 an ADVANCED COUNTER ROTATING DISK WING AIRCRAFT CONCEPT NIAC
Godwit Helicopter
Proposal for the 36Th Annual Design Competition As It Sees fit
1 Aerodynamic Study of a Small, Ducted VTOL Aerial Vehicle
Low-Tip-Speed High-Torque Proprotor Noise Approximation for Design Cycle Analysis
Large-Scale Wind-Tunru L Studies of Several Vtol Types
Waterspout - Advanced Deployable Compact Rotorcraft in Support of Special Operation Forces
Helicopter Rotor Lift Distributions for Minimum Induced Power Loss by Kyle Yi-Ling Yang B.S
Design NASA Grant NAG 2-918
Radio Controlled Autogiro Aerodynamic Design
HELICOPTERS for LOGGING CHARACTERISTICS, OPERATION, and SAFETY Conslderations
AHS International's Igor I. Sikorsky
NDARC — NASA Design and Analysis of Rotorcraft Validation and Demonstration
A Vehicle Design and Optimization Model for On-Demand Aviation
Influence of Arbitrary Vortical Wake Evolution on Flowfield and Noise Generation of Helicopter Rotors
Aerodynamic Trade Study of Compound Helicopter Concepts
Civil Applications of High-Speed Rotorcraft and Powered-Lift Aircraft Configurations
The Aircraft, the Rotorcraft and the Life of Walter Rieseler 1890-1937 Berend G
DEVELOPMENT of a SIMPLIFIED INFLOW MODEL for a HELICOPTER ROTOR in DESCENT FLIGHT Chang Chen
Performance Analysis of a Coaxial Helicopter in Hover and Forward Flight
Build Them and You Will Learn — Bell V-280 Valor
Electric VTOL Configurations Comparison
Design and Performance of Lift-Offset Rotorcraft for Short-Haul Missions
Effects of Disk Loading on Handling Qualities of Large-Scale, Variable-RPM Quadcopters