• Register
  • Login

European Journal of Molecular & Clinical Medicine

  1. Home
  2. TRANSIENT EFFECT OF AIRCRAFT PROPELLER BLADE BY USING COMPOSITES

Current Issue

By Issue

By Author

By Subject

Author Index

Keyword Index

About Journal

Aims and Scope

Editorial Board

Publication Ethics

Indexing and Abstracting

Related Links

FAQ

Peer Review Process

Journal Metrics

News

TRANSIENT EFFECT OF AIRCRAFT PROPELLER BLADE BY USING COMPOSITES

    Author

    • KAKUMANI DHARMATEJA AJAY KUMAR REVURI

    India

,

Document Type : Research Article

  • Article Information
  • Download
  • Export Citation
  • Statistics
  • Share

Abstract

A propeller is a fan form which transmits power by turning rotational movement into an impeller. The pressure differential between the airfoil formed blade's surfaces in front and rear is created and the fluid is propelled behind the blade, for example air. The present analysis is directed to the examination of the function of the composite propeller and its terms, simulation and the simulation of the flow of the composite propeller of the aircraft. For study of ANSYS applications integrated aircraft propeller. The deformity, tension and pressure of the composite propeller blade must be calculated by static and dynamic analysis. Tiredness analysis to calculate the component's existence. The propeller blades that differ in no of blades are optimised for 2,3&5 blades and even E-glass material epoxy, aluminium alloy and carbon epoxy have been optimised. CATIA parametric machine simulation 3D. 3D.

  • XML
  • PDF 283.45 K
  • RIS
  • EndNote
  • Mendeley
  • BibTeX
  • APA
  • MLA
  • HARVARD
  • VANCOUVER
    • Article View: 256
    • PDF Download: 607
European Journal of Molecular & Clinical Medicine
Volume 7, Issue 10
December 2020
Page 2491-2497
Files
  • XML
  • PDF 283.45 K
Share
Export Citation
  • RIS
  • EndNote
  • Mendeley
  • BibTeX
  • APA
  • MLA
  • HARVARD
  • VANCOUVER
Statistics
  • Article View: 256
  • PDF Download: 607

APA

AJAY KUMAR REVURI, K. D. (2021). TRANSIENT EFFECT OF AIRCRAFT PROPELLER BLADE BY USING COMPOSITES. European Journal of Molecular & Clinical Medicine, 7(10), 2491-2497.

MLA

KAKUMANI DHARMATEJA AJAY KUMAR REVURI. "TRANSIENT EFFECT OF AIRCRAFT PROPELLER BLADE BY USING COMPOSITES". European Journal of Molecular & Clinical Medicine, 7, 10, 2021, 2491-2497.

HARVARD

AJAY KUMAR REVURI, K. D. (2021). 'TRANSIENT EFFECT OF AIRCRAFT PROPELLER BLADE BY USING COMPOSITES', European Journal of Molecular & Clinical Medicine, 7(10), pp. 2491-2497.

VANCOUVER

AJAY KUMAR REVURI, K. D. TRANSIENT EFFECT OF AIRCRAFT PROPELLER BLADE BY USING COMPOSITES. European Journal of Molecular & Clinical Medicine, 2021; 7(10): 2491-2497.

  • Home
  • About Journal
  • Editorial Board
  • Submit Manuscript
  • Contact Us
  • Glossary
  • Sitemap

News

 

For Special Issue Proposal : editor.ejmcm21@gmail.com

Newsletter Subscription

Subscribe to the journal newsletter and receive the latest news and updates

© Journal Management System. Powered by ejournalplus