Now showing items 1-10 of 17
Velocity measurements near the blade tip and in the tip vortex core of a hovering model rotor
(Georgia Institute of Technology, 1986-12)
The normal component of the induced velocity near a vortex ring and its application to lifting rotor problems
(Georgia Institute of Technology, 1951-12)
A linear system identification and validaton of an AH-64 apache aeroelastic simulation model
(Georgia Institute of Technology, 1993-08)
A method for the efficient calculation of elastic rotor blade dynamic response in forward flight
(Georgia Institute of Technology, 1987-05)
A fourth order Euler/Navier-Stokes prediction method for the aerodynamics and aeroelasticity of hovering rotor blades
(Georgia Institute of Technology, 1994-05)
Investigation of a stop-fold tiltrotor
(Georgia Institute of Technology, 2009-07-09)
In 1967 the US Air Force solicited proposals for ``low-disc-loading [Vertical Takeoff and Landing] configurations suitable for high speed flight.' Bell Helicopter elected to respond with a proposal after initial analysis ...
A multi-fidelity framework for physics based rotor blade simulation and optimization
(Georgia Institute of Technology, 2008-11-17)
New helicopter rotor designs are desired that offer increased efficiency, reduced vibration, and reduced noise. This problem is multidisciplinary, requiring knowledge of structural dynamics, aerodynamics, and aeroacoustics. ...
Computational fluid dynamic studies of high lift rotor systems using distributed computing
(Georgia Institute of Technology, 1995-05)
Development of computer codes for analysis of rotorcraft aerodynamics
(Georgia Institute of Technology, 1986)
Using tightly-coupled CFD/CSD simulation for rotorcraft stability analysis
(Georgia Institute of Technology, 2012-01-17)
Dynamic stall deeply affects the response of helicopter rotor blades, making its modeling accuracy very important. Two commonly used dynamic stall models were implemented in a comprehensive code, validated, and contrasted ...