Modeling the Coupled Rotor/Fuselage Response of the H-3 Sea King Utilizing the NPS Full Nonlinear Response pdf epub fb2

Modeling the Coupled Rotor/Fuselage Response of the H-3 Sea King Utilizing the NPS Full Nonlinear Response by Salvatore P. Rafanello pdf epub fb2

Modeling the Coupled Rotor/Fuselage Response of the H-3 Sea King Utilizing the NPS Full Nonlinear Response Author: Salvatore P. Rafanello
Title: Modeling the Coupled Rotor/Fuselage Response of the H-3 Sea King Utilizing the NPS Full Nonlinear Response
ISBN: 1423545605
ISBN13: 978-1423545606
Other Formats: rtf azw mobi lrf
Pages: -
Publisher: Storming Media (1999)
Language: English
Category: No category
Size PDF version: 1267 kb
Size EPUB version: 1748 kb
Subcategory: -




This is a NAVAL POSTGRADUATE SCHOOL MONTEREY CA report procured by the Pentagon and made available for public release. It has been reproduced in the best form available to the Pentagon. It is not spiral-bound, but rather assembled with Velobinding in a soft, white linen cover. The Storming Media report number is A428163. The abstract provided by the Pentagon follows: Adapting the Naval Postgraduate School full nonlinear simulation model of coupled rotor/fuselage response to the 11-3 Sea King, the concentration of this work rests on validating the rotor simulation against an actual rotorcraft. The parameters of the 11-3 from the characteristic equation of a modeled mass-spring- damper system are inputted into a five-bladed model initially utilizing MAPLE to process LaGrange's equation defining the helicopter's full set of nonlinear equations of motion. Results are converted to MATLAB and are then processed in SIMULINK returning time history plots of blade/ fuselage motion. Conclusions are in accordance with literature of Coleman, Fein old and Deutsch.