Now showing items 11-20 of 53
Analysis Of Computational Modeling Techniques For Complete Rotorcraft Configurations
(Georgia Institute of Technology, 2006-04-11)
Recent increases in computing power and memory have created renewed interest in alternative grid schemes such as unstructured grids, which facilitate rapid grid generation by relaxing restrictions on grid structure. Three ...
A linear system identification and validaton of an AH-64 apache aeroelastic simulation model
(Georgia Institute of Technology, 1993-08)
Preliminary Turboshaft Engine Design Methodology for Rotorcraft Applications
(Georgia Institute of Technology, 2006-11-20)
In the development of modern rotorcraft vehicles, many unique challenges emerge due to the highly coupled nature of individual rotorcraft design disciplines therefore, the use of an integrated product and process development ...
A method for the efficient calculation of elastic rotor blade dynamic response in forward flight
(Georgia Institute of Technology, 1987-05)
Study of an asymptotic method for helicopter rotor blade aerodynamic loads
(Georgia Institute of Technology, 1982-12)
An analytical method for the prediction of unsteady rotor/airframe interactions in forward flight
(Georgia Institute of Technology, 1988-08)
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. ...
Towards a unified analysis methodology for composite rotor blades
(Georgia Institute of Technology, 1989-08)