JETIREXPLORE- Search Thousands of research papers



Published in:

Volume 7 Issue 3
March-2020
eISSN: 2349-5162

Unique Identifier

JETIR2003030

Page Number

161-171

Share This Article


Title

MODELING AND ANALYSIS OF DISC ROTOR WING

ISSN

2349-5162

Cite This Article

"MODELING AND ANALYSIS OF DISC ROTOR WING", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.7, Issue 3, page no.161-171, March-2020, Available :http://www.jetir.org/papers/JETIR2003030.pdf

Abstract

Disc rotor configuration may be a conceptual design. the aim of the Project is to guage the merits of the DiscRotor concept that combine the features of a retractable rotor system for vertical take-off and landing (VTOL) with an integral, circular wing for high-speed flight. The primary objective of this project is to style such a configuration using the planning software Unigraphics and afterward analyzing the designed structure for its structural strength in analysis software ANSYS. This project deals with the all the required aerodynamic requirements of the rotor configuration. In today’s world most the vtol/stol largely depends upon the thrust vectoring that needs huge amounts of fuel and separate devices like nozzles etc., whose production is extremely much tedious and dear. this is often an effort to use a rotor as within the case of helicopters for vtol/stol thus reducing the foremost of the value though weight would be considered as a hindrance to the project.

Key Words

Disc rotor wing, vertical take-off and landing (VTOL), UNIGRAPHICS, ANSYS software, Force, Coefficients, Wall and Wing.

Cite This Article

"MODELING AND ANALYSIS OF DISC ROTOR WING", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.7, Issue 3, page no. pp161-171, March-2020, Available at : http://www.jetir.org/papers/JETIR2003030.pdf

Publication Details

Published Paper ID: JETIR2003030
Registration ID: 229379
Published In: Volume 7 | Issue 3 | Year March-2020
DOI (Digital Object Identifier):
Page No: 161-171
ISSN Number: 2349-5162

Download Paper

Preview Article

Download Paper




Cite This Article

"MODELING AND ANALYSIS OF DISC ROTOR WING", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.7, Issue 3, page no. pp161-171, March-2020, Available at : http://www.jetir.org/papers/JETIR2003030.pdf




Preview This Article


Downlaod

Click here for Article Preview

Download PDF

Downloads

00064

Print This Page

Current Call For Paper