University of Anbar
  • Register
  • Login

Anbar Journal of Engineering Sciences

Notice

As part of Open Journals’ initiatives, we create website for scholarly open access journals. If you are responsible for this journal and would like to know more about how to use the editorial system, please visit our website at https://ejournalplus.com or
send us an email to info@ejournalplus.com

We will contact you soon

  1. Home
  2. Volume 3, Issue 2
  3. Authors

Current Issue

By Issue

By Subject

Keyword Index

Author Index

Indexing Databases XML

About Journal

Aims and Scope

Editorial Board

Publication Ethics

Indexing and Abstracting

Related Links

Peer Review Process

News

Facts and Figures

Reviewers in AJES

Theoretical and Experimental Study of a Forward Swept Wing

    Hayder M. Jaffal A. S. Darwish Ibtisam A. Hassan

Anbar Journal of Engineering Sciences, 2010, Volume 3, Issue 2, Pages 15-30
10.37649/aengs.2010.14202

  • Show Article
  • Download
  • Cite
  • Statistics
  • Share

Abstract

The aerodynamic characteristics of forward swept wing were studied theoretically and experimentally .In the present work, theoretically a computer program was constructed to predict the pressure distribution about surface of the wing using three dimensional Low Order Subsonic Panel method. The aerodynamic coefficients of the wing were calculated from the pressure distribution which gained from tangential velocities Experimentally ,test were carried out by designing and manufacturing a wing model with special arrangement for pressure tapping, suitable for low wind tunnel testing. The entire wing was rotated rotate about an axis in the plane of symmetry and normal to the chord to produce different sweep and incidence angles for wing, by using rotating mechanism. Wind tunnel test was carried out at (Uپ‡=33.23m/s) for different swept angles and angles of attack.Comparisons were made between the predicted and experimental results. It is good and gave reasonable closeness. It was clear from the present investigation that the lift and drag characteristics for the forward swept wing are less in values compared with the swept back wing, therefore a forward swept wing can fly at higher speed corresponding to a pressure distribution associated for lower speed.
Keywords:
    Forward Swept angles Wing Aerodynamic characteristics
  • PDF (1829 K)
  • XML
(2010). Theoretical and Experimental Study of a Forward Swept Wing. Anbar Journal of Engineering Sciences, 3(2), 15-30. doi: 10.37649/aengs.2010.14202
Hayder M. Jaffal; A. S. Darwish; Ibtisam A. Hassan. "Theoretical and Experimental Study of a Forward Swept Wing". Anbar Journal of Engineering Sciences, 3, 2, 2010, 15-30. doi: 10.37649/aengs.2010.14202
(2010). 'Theoretical and Experimental Study of a Forward Swept Wing', Anbar Journal of Engineering Sciences, 3(2), pp. 15-30. doi: 10.37649/aengs.2010.14202
Theoretical and Experimental Study of a Forward Swept Wing. Anbar Journal of Engineering Sciences, 2010; 3(2): 15-30. doi: 10.37649/aengs.2010.14202
  • RIS
  • EndNote
  • BibTeX
  • APA
  • MLA
  • Harvard
  • Vancouver
  • Article View: 72
  • PDF Download: 23
  • LinkedIn
  • Twitter
  • Facebook
  • Google
  • Telegram
  • Home
  • Glossary
  • News
  • Aims and Scope
  • Privacy Policy
  • Sitemap

This journal is licensed under a Creative Commons Attribution-NonCommercial 4.0 International (CC BY-NC 4.0)

This journal is licensed under a Creative Commons Attribution 4.0 International (CC-BY 4.0)

Powered by eJournalPlus